예제 #1
0
// Default settings
static void resetConf(void)
{
    int i;
    int8_t servoRates[8] = { 30, 30, 100, 100, 100, 100, 100, 100 };

    // Clear all configuration
    memset(&mcfg, 0, sizeof(master_t));
    memset(&cfg, 0, sizeof(config_t));

    mcfg.version = EEPROM_CONF_VERSION;
    mcfg.mixerConfiguration = MULTITYPE_QUADX;
    featureClearAll();
#ifdef CJMCU
    featureSet(FEATURE_PPM);
#else
    featureSet(FEATURE_VBAT);
#endif

    // global settings
    mcfg.current_profile = 0;       // default profile
    mcfg.gyro_cmpf_factor = 600;    // default MWC
    mcfg.gyro_cmpfm_factor = 250;   // default MWC
    mcfg.gyro_lpf = 42;             // supported by all gyro drivers now. In case of ST gyro, will default to 32Hz instead
    mcfg.accZero[0] = 0;
    mcfg.accZero[1] = 0;
    mcfg.accZero[2] = 0;
    mcfg.gyro_align = ALIGN_DEFAULT;
    mcfg.acc_align = ALIGN_DEFAULT;
    mcfg.mag_align = ALIGN_DEFAULT;
    mcfg.board_align_roll = 0;
    mcfg.board_align_pitch = 0;
    mcfg.board_align_yaw = 0;
    mcfg.acc_hardware = ACC_DEFAULT;     // default/autodetect
    mcfg.mag_hardware = MAG_DEFAULT;
    mcfg.max_angle_inclination = 500;    // 50 degrees
    mcfg.yaw_control_direction = 1;
    mcfg.moron_threshold = 32;
    mcfg.currentscale = 400; // for Allegro ACS758LCB-100U (40mV/A)
    mcfg.vbatscale = 110;
    mcfg.vbatmaxcellvoltage = 43;
    mcfg.vbatmincellvoltage = 33;
    mcfg.vbatwarningcellvoltage = 35;
    mcfg.power_adc_channel = 0;
    mcfg.serialrx_type = 0;
    mcfg.spektrum_sat_bind = 0;
    mcfg.telemetry_provider = TELEMETRY_PROVIDER_FRSKY;
    mcfg.telemetry_port = TELEMETRY_PORT_UART;
    mcfg.telemetry_switch = 0;
    mcfg.midrc = 1500;
    mcfg.mincheck = 1100;
    mcfg.maxcheck = 1900;
    mcfg.retarded_arm = 0;       // disable arm/disarm on roll left/right
    mcfg.disarm_kill_switch = 1; // AUX disarm independently of throttle value
    mcfg.fw_althold_dir = 1;
    // Motor/ESC/Servo
    mcfg.minthrottle = 1150;
    mcfg.maxthrottle = 1850;
    mcfg.mincommand = 1000;
    mcfg.deadband3d_low = 1406;
    mcfg.deadband3d_high = 1514;
    mcfg.neutral3d = 1460;
    mcfg.deadband3d_throttle = 50;
    mcfg.motor_pwm_rate = MOTOR_PWM_RATE;
    mcfg.servo_pwm_rate = 50;
    // safety features
    mcfg.auto_disarm_board = 5; // auto disarm after 5 sec if motors not started or disarmed
    // gps/nav stuff
    mcfg.gps_type = GPS_NMEA;
    mcfg.gps_baudrate = GPS_BAUD_115200;
    // serial (USART1) baudrate
    mcfg.serial_baudrate = 115200;
    mcfg.softserial_baudrate = 9600;
    mcfg.softserial_1_inverted = 0;
    mcfg.softserial_2_inverted = 0;
    mcfg.looptime = 3500;
    mcfg.emf_avoidance = 0;
    mcfg.rssi_aux_channel = 0;
    mcfg.rssi_adc_max = 4095;

    cfg.pidController = 0;
    cfg.P8[ROLL] = 40;
    cfg.I8[ROLL] = 30;
    cfg.D8[ROLL] = 23;
    cfg.P8[PITCH] = 40;
    cfg.I8[PITCH] = 30;
    cfg.D8[PITCH] = 23;
    cfg.P8[YAW] = 85;
    cfg.I8[YAW] = 45;
    cfg.D8[YAW] = 0;
    cfg.P8[PIDALT] = 50;
    cfg.I8[PIDALT] = 0;
    cfg.D8[PIDALT] = 0;
    cfg.P8[PIDPOS] = 11; // POSHOLD_P * 100;
    cfg.I8[PIDPOS] = 0; // POSHOLD_I * 100;
    cfg.D8[PIDPOS] = 0;
    cfg.P8[PIDPOSR] = 20; // POSHOLD_RATE_P * 10;
    cfg.I8[PIDPOSR] = 8; // POSHOLD_RATE_I * 100;
    cfg.D8[PIDPOSR] = 45; // POSHOLD_RATE_D * 1000;
    cfg.P8[PIDNAVR] = 14; // NAV_P * 10;
    cfg.I8[PIDNAVR] = 20; // NAV_I * 100;
    cfg.D8[PIDNAVR] = 80; // NAV_D * 1000;
    cfg.P8[PIDLEVEL] = 90;
    cfg.I8[PIDLEVEL] = 10;
    cfg.D8[PIDLEVEL] = 100;
    cfg.P8[PIDMAG] = 40;
    cfg.P8[PIDVEL] = 120;
    cfg.I8[PIDVEL] = 45;
    cfg.D8[PIDVEL] = 1;
    cfg.rcRate8 = 90;
    cfg.rcExpo8 = 65;
    cfg.yawRate = 0;
    cfg.dynThrPID = 0;
    cfg.tpa_breakpoint = 1500;
    cfg.thrMid8 = 50;
    cfg.thrExpo8 = 0;
    // for (i = 0; i < CHECKBOXITEMS; i++)
    //     cfg.activate[i] = 0;
    cfg.angleTrim[0] = 0;
    cfg.angleTrim[1] = 0;
    cfg.locked_in = 0;
    cfg.mag_declination = 0;    // For example, -6deg 37min, = -637 Japan, format is [sign]dddmm (degreesminutes) default is zero.
    cfg.acc_lpf_factor = 4;
    cfg.accz_deadband = 40;
    cfg.accxy_deadband = 40;
    cfg.baro_tab_size = 21;
    cfg.baro_noise_lpf = 0.6f;
    cfg.baro_cf_vel = 0.985f;
    cfg.baro_cf_alt = 0.965f;
    cfg.accz_lpf_cutoff = 5.0f;
    cfg.acc_unarmedcal = 1;
    cfg.small_angle = 25;

    // Radio
    parseRcChannels("AETR1234");
    cfg.deadband = 0;
    cfg.yawdeadband = 0;
    cfg.alt_hold_throttle_neutral = 40;
    cfg.alt_hold_fast_change = 1;
    cfg.throttle_correction_value = 0;      // could 10 with althold or 40 for fpv
    cfg.throttle_correction_angle = 800;    // could be 80.0 deg with atlhold or 45.0 for fpv

    // Failsafe Variables
    cfg.failsafe_delay = 10;                // 1sec
    cfg.failsafe_off_delay = 200;           // 20sec
    cfg.failsafe_throttle = 1200;           // decent default which should always be below hover throttle for people.
    cfg.failsafe_detect_threshold = 985;    // any of first 4 channels below this value will trigger failsafe

    // servos
    for (i = 0; i < 8; i++) {
        cfg.servoConf[i].min = 1020;
        cfg.servoConf[i].max = 2000;
        cfg.servoConf[i].middle = 1500;
        cfg.servoConf[i].rate = servoRates[i];
    }

    cfg.yaw_direction = 1;
    cfg.tri_unarmed_servo = 1;

    // gimbal
    cfg.gimbal_flags = GIMBAL_NORMAL;

    // gps/nav stuff
    cfg.gps_wp_radius = 200;
    cfg.gps_lpf = 20;
    cfg.nav_slew_rate = 30;
    cfg.nav_controls_heading = 1;
    cfg.nav_speed_min = 100;
    cfg.nav_speed_max = 300;
    cfg.ap_mode = 40;
    // fw stuff
    cfg.fw_roll_throw = 0.5f;
    cfg.fw_pitch_throw = 0.5f;
    cfg.fw_gps_maxcorr = 20;
    cfg.fw_gps_rudder = 15;
    cfg.fw_gps_maxclimb = 15;
    cfg.fw_gps_maxdive = 15;
    cfg.fw_climb_throttle = 1900;
    cfg.fw_cruise_throttle = 1500;
    cfg.fw_idle_throttle = 1300;
    cfg.fw_scaler_throttle = 8;
    cfg.fw_roll_comp = 1;
    // control stuff
    mcfg.reboot_character = 'R';

    // custom mixer. clear by defaults.
    for (i = 0; i < MAX_MOTORS; i++)
        mcfg.customMixer[i].throttle = 0.0f;

    // copy default config into all 3 profiles
    for (i = 0; i < 3; i++)
        memcpy(&mcfg.profile[i], &cfg, sizeof(config_t));
}
예제 #2
0
// Default settings
static void resetConf(void)
{
    uint8_t i;
    const int8_t default_align[3][3] = { /* GYRO */ { 0, 0, 0 }, /* ACC */ { 0, 0, 0 }, /* MAG */ { 0, 0, 0 } };
    memset(&cfg, 0, sizeof(config_t));

    cfg.version = EEPROM_CONF_VERSION;
    cfg.mixerConfiguration = MULTITYPE_QUADX;
    featureClearAll();
//    featureSet(FEATURE_VBAT);
    featureSet(FEATURE_PPM);
//    featureSet(FEATURE_FAILSAFE);
//    featureSet(FEATURE_LCD);
//    featureSet(FEATURE_GPS);
//    featureSet(FEATURE_PASS);                   // Just pass Throttlechannel
//    featureSet(FEATURE_SONAR);

    cfg.P8[ROLL]                  =  35;        // 40
    cfg.I8[ROLL]                  =  30;
    cfg.D8[ROLL]                  =  30;

    cfg.P8[PITCH]                 =  35;        // 40
    cfg.I8[PITCH]                 =  30;
    cfg.D8[PITCH]                 =  30;

    cfg.P8[YAW]                   =  60;        // 70
    cfg.I8[YAW]                   =  45;

    cfg.P8[PIDALT]                = 100;
    cfg.I8[PIDALT]                =  30;
    cfg.D8[PIDALT]                =  80;

    cfg.P8[PIDPOS]                =  10;        // FIND YOUR VALUE
    cfg.I8[PIDPOS]                =  40;        // USED

    cfg.P8[PIDPOSR]               =  70;        // FIND YOUR VALUE                    // Controls the speed part with my PH logic
    cfg.D8[PIDPOSR]               = 100;        // FIND YOUR VALUE                    // Controls the speed part with my PH logic

    cfg.P8[PIDNAVR]               =  15;        // 14 More ?
    cfg.I8[PIDNAVR]               =   0;        // NAV_I * 100;                       // Scaling/Purpose unchanged
    cfg.D8[PIDNAVR]               =   0;        // NAV_D * 1000;                      // Scaling/Purpose unchanged

//    cfg.P8[PIDPOS]                = 11;         // APM PH Stock values
//    cfg.I8[PIDPOS]                = 0;
//    cfg.D8[PIDPOS]                = 0;

//    cfg.P8[PIDPOSR]               = 20;         // POSHOLD_RATE_P * 10;
//    cfg.I8[PIDPOSR]               = 8;          // POSHOLD_RATE_I * 100;
//    cfg.D8[PIDPOSR]               = 45;         // POSHOLD_RATE_D * 1000;

//    cfg.P8[PIDNAVR]               = 14;         // NAV_P * 10;
//    cfg.I8[PIDNAVR]               = 20;         // NAV_I * 100;
//    cfg.D8[PIDNAVR]               = 80;         // NAV_D * 1000;

    cfg.P8[PIDLEVEL]              = 70;         // 70
    cfg.I8[PIDLEVEL]              = 10;
    cfg.D8[PIDLEVEL]              = 50;

    cfg.P8[PIDMAG]                = 80;         // cfg.P8[PIDVEL] = 0;// cfg.I8[PIDVEL] = 0;// cfg.D8[PIDVEL] = 0;

    cfg.rcRate8                   = 100;
    cfg.rcExpo8                   = 80;         // cfg.rollPitchRate = 0;// cfg.yawRate = 0;// cfg.dynThrPID = 0;
    cfg.thrMid8                   = 50;

    memcpy(&cfg.align, default_align, sizeof(cfg.align));

    cfg.mag_dec                   = 113;        // Crashpilot //cfg.acc_hdw = ACC_DEFAULT;// default/autodetect
    cfg.mag_time                  = 1;          // (1-6) Calibration time in minutes
    cfg.mag_gain                  = 0;          // 0(default) = 1.9 GAUSS ; 1 = 2.5 GAUSS (problematic copters, will reduce 20% resolution)
    cfg.acc_hdw                   = 2;          // Crashpilot MPU6050
    cfg.acc_lpfhz                 = 10.0f;      // [0.x-100Hz] LPF for angle/horizon 0.536f resembles somehow the orig mwii factor
    cfg.acc_altlpfhz              = 15;         // [1-100Hz]   LPF for althold
    cfg.acc_gpslpfhz              = 30;         // [1-100Hz]   LPF for GPS ins stuff
    cfg.looptime                  = 3000;
    cfg.mainpidctrl               = 0;          // 0 = OriginalMwiiPid pimped by me, 1 = New mwii controller (experimental, float pimped + pt1)
    cfg.maincuthz                 = 12;         // [1-100Hz] Cuf Off Frequency for D term of main Pid controller
    cfg.gpscuthz                  = 45;         // [1-100Hz] Cuf Off Frequency for D term of GPS Pid controller 

    cfg.gy_gcmpf                  = 700;        // (10-1000) 400 default. Now 1000. The higher, the more weight gets the gyro and the lower is the correction with Acc data.
    cfg.gy_mcmpf                  = 200;        // (10-2000) 200 default for 10Hz. Now higher. Gyro/Magnetometer Complement.
    cfg.gy_smrll                  = 0;
    cfg.gy_smptc                  = 0;
    cfg.gy_smyw                   = 0;          // In Tricopter mode a "1" will enable a moving average filter, anything higher will also enable a lowpassfilter
    cfg.gy_lpf                    = 42;         // Values for MPU 6050/3050: 256, 188, 98, 42, 20, 10, (HZ) For L3G4200D: 93, 78, 54, 32
    cfg.gy_stdev                  = 5;

    // Baro
    cfg.accz_vcf                  = 0.985f;     // Crashpilot: Value for complementary filter accz and barovelocity
    cfg.accz_acf                  = 0.960f;     // Crashpilot: Value for complementary filter accz and altitude
    cfg.bar_lag                   = 0.3f;       // Lag of Baro/Althold stuff in general, makes stop in hightchange snappier
    cfg.bar_dscl                  = 0.7f;       // Scale downmovement down (because copter drops faster than rising)
    cfg.bar_dbg                   = 0;          // Crashpilot: 1 = Debug Barovalues //cfg.baro_noise_lpf = 0.6f;// Crashpilot: Not used anymore//cfg.baro_cf = 0.985f;// Crashpilot: Not used anymore

    // Autoland
    cfg.al_barolr                 = 50;         // [10 - 200cm/s] Baro Landingrate
    cfg.al_snrlr                  = 50;         // [10 - 200cm/s] Sonar Landingrate - You can specify different landingfactor here on sonar contact, because sonar land maybe too fast when snr_cf is high
    cfg.al_debounce               = 5;          // (0-20%) 0 Disables. Defines a Throttlelimiter on Autoland. Percentage defines the maximum deviation of assumed hoverthrottle during Autoland
    cfg.al_tobaro                 = 2000;       // Timeout in ms (100 - 5000) before shutoff on autoland. "esc_nfly" must be undershot for that timeperiod
    cfg.al_tosnr                  = 1000;       // Timeout in ms (100 - 5000) If sonar aided land is wanted (snr_land = 1) you can choose a different timeout here

    // Autostart
    cfg.as_lnchr                  = 200;        // [50 - 250 no dimension DEFAULT:200] Autostart initial launchrate to get off the ground. When as_stdev is exceeded, as_clmbr takes over
    cfg.as_clmbr                  = 100;        // [50 - 250cm/s DEFAULT:100] Autostart climbrate in cm/s after liftoff! Autostart Rate in cm/s will be lowered when approaching targethight.
    cfg.as_trgt                   = 0;          // [0 - 255m  DEFAULT:0 (0 = Disable)] Autostart Targethight in m Note: use 2m or more
    cfg.as_stdev                  = 10;         // [5 - 20 no dimension DEFAULT:10] This is the std. deviation of the variometer when a liftoff is assumed. The higher the more unsensitive.

    cfg.vbatscale                 = 110;
    cfg.vbatmaxcellvoltage        = 43;
    cfg.vbatmincellvoltage        = 33;
    cfg.power_adc_channel         = 0;

    // Radio
    parseRcChannels("AETR1234");
    cfg.rc_db                     = 20;         // Crashpilot: A little deadband will not harm our crappy RC
    cfg.rc_dbyw                   = 20;         // Crashpilot: A little deadband will not harm our crappy RC
    cfg.rc_dbah                   = 50;         // Crashpilot: A little deadband will not harm our crappy RC
    cfg.rc_dbgps                  = 5;          // Additional Deadband for all GPS functions;
    cfg.devorssi                  = 0;          // Will take the last channel for RSSI value, so add one to rc_auxch, don't use that auxchannel unless you want it to trigger something
                                                // Note Spektrum or Graupner will override that setting to 0.
    cfg.rssicut                   = 0;          // [0-80%][0 Disables] Below that percentage rssi will show zero.
    // cfg.spektrum_hires = 0;
    cfg.rc_minchk                 = 1100;
    cfg.rc_mid                    = 1500;
    cfg.rc_maxchk                 = 1900;
    cfg.rc_lowlat                 = 1;          // [0 - 1] Default 1. 1 = lower latency, 0 = normal latency/more filtering.
    cfg.rc_rllrm                  = 0;          // disable arm/disarm on roll left/right
    cfg.rc_auxch                  = 4;          // [4 - 6] cGiesen: Default = 4, then like the standard! Crashpilot: Limited to 6 aux for safety
    cfg.rc_killt                  = 0;          // Time in ms when your arm switch becomes a Killswitch, 0 disables the Killswitch, can not be used together with FEATURE_INFLIGHT_ACC_CAL
    cfg.rc_flpsp                  = 0;          // [0-3] When enabled(1) and upside down in acro or horizon mode throttle is reduced (see readme)
    cfg.rc_motor                  = 0;          // [0-2] Behaviour when thr < rc_minchk: 0= minthrottle no regulation, 1= minthrottle&regulation, 2= Motorstop 

    // Motor/ESC/Servo
    cfg.esc_gain                  =    0;       // [0Disables - 32] Gain for esc to reduce delay 16 = Gain of 1 that would double the initial response(limited to +500) Only helps unflashed ESC.
//  cfg.esc_min                   = 1150;       // ORIG
    cfg.esc_min                   = 1100;
    cfg.esc_max                   = 1950;
    cfg.esc_moff                  = 1000;
    cfg.esc_nfly                  = 1300;       // This is the absolute throttle that kicks off the "has landed timer" if it is too low cfg.rc_minchk + 5% is taken. Also baselinethr for Autostart, also plausibility check for initial Failsafethrottle
//  cfg.esc_nfly                  = 0;          // This is the absolute throttle that kicks off the "has landed timer" if it is too low cfg.rc_minchk + 5% is taken.
    cfg.esc_pwm                   = 400;
    cfg.srv_pwm                   = 50;
    cfg.pass_mot                  = 0;          // Crashpilot: Only used with feature pass. If 0 = all Motors, otherwise specific Motor

    // servos
    cfg.tri_ydir                  = 1;
    cfg.tri_ymid                  = 1500;
    cfg.tri_ymin                  = 1020;
    cfg.tri_ymax                  = 2000;
    cfg.tri_ydel                  = 0;          // [0-1000ms] Tri Yaw Arm delay: Time in ms after wich the yaw servo after arming will engage (useful with "yaw arm"). 0 disables Yawservo always active.

    // flying wing
    cfg.wing_left_min             = 1020;
    cfg.wing_left_mid             = 1500;
    cfg.wing_left_max             = 2000;
    cfg.wing_right_min            = 1020;
    cfg.wing_right_mid            = 1500;
    cfg.wing_right_max            = 2000;
    cfg.pitch_direction_l         = 1;
    cfg.pitch_direction_r         = -1;
    cfg.roll_direction_l          = 1;
    cfg.roll_direction_r          = 1;

    // gimbal
    cfg.gbl_pgn                   = 10;
    cfg.gbl_rgn                   = 10;
    cfg.gbl_flg                   = GIMBAL_NORMAL;
    cfg.gbl_pmn                   = 1020;
    cfg.gbl_pmx                   = 2000;
    cfg.gbl_pmd                   = 1500;
    cfg.gbl_rmn                   = 1020;
    cfg.gbl_rmx                   = 2000;
    cfg.gbl_rmd                   = 1500;

    // gps/nav
    cfg.gps_type                  = 1;          // GPS_NMEA = 0, GPS_UBLOX = 1, GPS_MTK16 = 2, GPS_MTK19 = 3, GPS_UBLOX_DUMB = 4
    cfg.gps_baudrate              = 115200;     //38400; // Changed 8/6/13 to 115200;
    cfg.gps_ins_vel               = 0.6f;       // Crashpilot GPS INS The LOWER the value the closer to gps speed // Dont go to high here
    cfg.gps_lag                   = 2000;       // GPS Lag in ms
    cfg.gps_ph_minsat             = 6;          // Minimal Satcount for PH, PH on RTL is still done with 5Sats or more
    cfg.gps_expo                  = 20;         // 1 - 99 % defines the actual Expo applied for GPS
    cfg.gps_ph_settlespeed        = 10;         // 1 - 200 cm/s PH settlespeed in cm/s
    cfg.gps_ph_brakemaxangle      = 15;         // 1 - 45 Degree Maximal Overspeedbrake
    cfg.gps_ph_minbrakepercent    = 50;         // 1 - 99% minimal percent of "brakemaxangle" left over for braking. Example brakemaxangle = 6 so 50 Percent is 3..
    cfg.gps_ph_brkacc             = 40;         // [1 - 500] Is the assumed negative braking acceleration in cm/(s*s) of copter. Value is positive though. It will be a timeout. The lower the Value the longe the Timeout
    cfg.gps_maxangle              = 35;         // 10 - 45 Degree Maximal over all GPS bank angle
    cfg.gps_wp_radius             = 200;
//  cfg.rtl_mnh                   = 20;         // (0 - 200m) Minimal RTL hight in m, 0 disables feature
	  cfg.rtl_mnh                   = 0;          // (0 - 200m) Minimal RTL hight in m, 0 disables feature
    cfg.rtl_cr                    = 80;         // [10 - 200cm/s] When rtl_mnh is defined this is the climbrate in cm/s
    cfg.rtl_mnd                   = 0;          // 0 Disables. Minimal distance for RTL in m, otherwise it will just autoland, prevent Failsafe jump in your face, when arming copter and turning off TX
    cfg.gps_rtl_flyaway           = 0;          // [0 - 100m] 0 Disables. If during RTL the distance increases beyond this value (in meters relative to RTL activation point), something is wrong, autoland

    cfg.gps_yaw                   = 30;         // Thats the MAG P during GPS functions, substitute for "cfg.P8[PIDMAG]"
    cfg.nav_rtl_lastturn          = 1;          // 1 = when copter gets to home position it rotates it's head to takeoff direction independend of nav_controls_heading
    cfg.nav_tail_first            = 0;          // 1 = Copter comes back with ass first (only works with nav_controls_heading = 1)
    cfg.nav_controls_heading      = 0;          // 1 = Nav controls YAW during WP ONLY
//  cfg.nav_controls_heading      = 1;          // 1 = Nav controls YAW during WP ONLY
    cfg.nav_speed_min             = 100;        // 10 - 200 cm/s don't set higher than nav_speed_max! That dumbness is not covered.
    cfg.nav_speed_max             = 350;        // 50 - 2000 cm/s don't set lower than nav_speed_min! That dumbness is not covered.
    cfg.nav_approachdiv           = 3;          // 2 - 10 This is the divisor for approach speed for wp_distance. Example: 400cm / 3 = 133cm/s if below nav_speed_min it will be adjusted
    cfg.nav_tiltcomp              = 30;         // 0 - 100 (20 TestDefault) Only arducopter really knows. Dfault was 54. This is some kind of a hack of them to reach actual nav_speed_max. 54 was Dfault, 0 disables
    cfg.nav_ctrkgain              = 0.5f;       // 0 - 10.0 (0.5 TestDefault) (Floatvariable) That is the "Crosstrackgain" APM Dfault is "1". "0" disables

    // Failsafe Variables
    cfg.fs_delay                  = 10;         // in 0.1s (10 = 1sec)
    cfg.fs_ofdel                  = 200;        // in 0.1s (200 = 20sec)
    cfg.fs_rcthr                  = 1200;       // decent Dfault which should always be below hover throttle for people.
    cfg.fs_ddplt                  = 0;		      // EXPERIMENTAL Time in sec when FS is engaged after idle on THR/YAW/ROLL/PITCH, 0 disables max 250
    cfg.fs_jstph                  = 0;          // Does just PH&Autoland an not RTL, use this in difficult areas with many obstacles to avoid RTL crash into something
    cfg.fs_nosnr                  = 1;          // When snr_land is set to 1, it is possible to ignore that on Failsafe, because FS over a tree could turn off copter

    // serial (USART1) baudrate
    cfg.serial_baudrate           = 115200;
    cfg.tele_prot                 = 0;          // Protocol ONLY used when Armed including Baudchange if necessary. 0 (Dfault)=Keep Multiwii @CurrentUSB Baud, 1=Frsky @9600Baud, 2=Mavlink @CurrentUSB Baud, 3=Mavlink @57KBaud (like stock minimOSD wants it)

    // LED Stuff
    cfg.LED_invert                = 0;          // Crashpilot: Inversion of LED 0&1 Partly implemented because Bootup is not affected
    cfg.LED_Type                  = 1;		      // 1=MWCRGB / 2=MONO_LED / 3=LEDRing
    cfg.LED_Pinout                = 1;		      // rc6
    cfg.LED_ControlChannel        = 8;		      // AUX4 (Channel 8)
    cfg.LED_Armed                 = 0;		      // 0 = Show LED only if armed, 1 = always show LED
    cfg.LED_Pattern1			        = 1300; 		  // 32bit bit pattern to have flickering led patterns / the pattern for MWCRGB 1000-2000
    cfg.LED_Pattern2			        = 1800; 		  // 32bit bit pattern to have flickering led patterns / the pattern for MWCRGB 1000-2000
    cfg.LED_Pattern3			        = 1900; 		  // 32bit bit pattern to have flickering led patterns / the pattern for MWCRGB 1000-2000
    cfg.LED_Toggle_Delay1         = 0x08;       // slow down LED_Pattern
    cfg.LED_Toggle_Delay2         = 0x08;       // slow down LED_Pattern
    cfg.LED_Toggle_Delay3         = 0x08;       // slow down LED_Pattern

    // SONAR
    // SOME INFO ON SONAR:
    // PWM56 are 5V resistant, RC78 only tolerate 3.3V(!!) so add a 1K Ohms resistor!!!
    // Note: You will never see the maximum possible sonar range in a copter, so go for the half of it (or less?)
    //
    // Connection possibilities depending on Receivertype:
    // PPSUM: RC78 possible, PWM56 possible (on max. quadcopters, see below)
    // Normal RX: Just Connection on Motorchannel 5&6 (PWM56) is possible.
    // The PWM56 sonar connection option is only available in setups with max motors 4, otherwise sonar is not initialized.
    //
    // HC-SR04:
    // Operation Voltage: 5V (!! Use PWM56 or 1K resistor !!)
    // Range: 2cm - 400cm
    // Angle: 15 Degrees (Test out for yourself: cfg.snr_tilt = X)
    //
    // Maxbotix in general
    // Operation Voltage: (some 2.5V)3.3V - 5V ((!! Use PWM56 or resistor with 5V !!)
    // Only wire the Maxbotics for PWM output (more precise anyway), not the analog etc. modes, just wire echopin (normally pin 2)
    // Range: 20cm(!) - 765cm (some >1000cm), MaxTiltAngle is not specified, depending on Model
    // Tested on MB1200 XL-MaxSonar-EZ0
    //
    // I2C sonar in general (by mj666)
    // If operation voltage of the sonar sensor is 5 Volt (NAZE I2C is 3.3 Volt), take care they do not have pull up resistors connected to 5 Volt.
    // Outputs are always open drain so there is no risk kill something only signals may be critical so keep wires short as possible.
    // Maxbotix I2CXL series operates with 3.3 and 5 Volt but 5Volt are preferred for best performance and stability.
    //
    // Devantech Ltd. (SRF02, SRF235, SRF08, SRF10):
    // Type; Range; Cycletime; Angle; Comment
    // SRF02; 16 to 600cm; 65ms; 55 degree; automatic calibration, minimum rage can be read from sensor (not implemented)
    // SRF235; 10 - 1200cm; 10ms; 15 degree; angle is may be to small for the use case
    // SRF08; 3 - 600cm; 65ms; 55 degree; range, gain an cycletime can be adjusted, multiple echos are measured (both not implemented)
    // SRF10; 6 - 600cm; 65ms; 72 degree; range, gain an cycletime can be adjusted (not implemented)
    // be sure to adjust settings accordingly, no additional test are done.
    // more details at: http://www.robot-electronics.co.uk/index.html
    //
    // Maxbotix I2CXL (MB1202, MB1212, MB1222, MB1232, MB1242)
    // I"CXL Series of sensors only differentiated by the beam pattern and sensibility. Maxbotix is recommending the MX1242 for quadcopter applications. The interface is always the same
    // NOTE: Maxbotix Sonars only operate with lower I2C speed, so the speed is changed on the fly during Maxbotix readout.
    // Thanks must go to mj666 for implementing that!
    // GENERAL WARNING: DON'T SET snr_min TOO LOW, OTHERWISE THE WRONG SONARVALUE WILL BE TAKEN AS REAL MEASUREMENT!!
    // I implemented some checks to prevent that user error, but still keep that in mind.
    // Min/Max are checked and changed if they are too stupid for your sonar. So if you suddenly see other values, thats not an eeprom error or so.
    // MAXBOTICS: SET snr_min to at least 30! I check this in sensors and change the value, if needed.
    // NOTE: I limited Maxbotics to 7 meters in the code, knowing that some types will do >10m, if you have one of them 7m is still the limit for you.
    // HC-SR04:   SET snr_min to at least 10 ! I check this in sensors and change the value, if needed.
    // DaddyWalross Sonar: I DON'T KNOW! But it uses HC-SR04 so i apply the same limits (10cm-400cm) to its output
    // Sonar minimal hight must be higher (including temperature difference) than the physical lower limit of the sensor to do a proximity alert
    // NOTE: Sonar is def. not a must - have. But nice to have.
    cfg.snr_type                  = 3;          // 0=PWM56 HC-SR04, 1=RC78 HC-SR04, 2=I2C(DaddyWalross), 3=MBPWM56, 4=MBRC78, 5=I2C(SRFxx), 6=I2C (MX12x2)
    cfg.snr_min                   = 30;         // Valid Sonar minimal range in cm (10 - 200) see warning above
    cfg.snr_max                   = 200;        // Valid Sonar maximal range in cm (50 - 700)
    cfg.snr_dbg                   = 0;          // 1 Sends Sonardata (within defined range and tilt) to debug[0] and tiltvalue to debug[1], debug[0] will be -1 if out of range/tilt. debug[2] contains raw sonaralt, like before
    cfg.snr_tilt                  = 18;         // Somehow copter tiltrange in degrees (Not exactly but good enough. Value * 0.9 = realtilt) in wich Sonar is possible
    cfg.snr_cf                    = 0.5f;       // The bigger, the more Sonarinfluence, makes switch between Baro/Sonar smoother and defines baroinfluence when sonarcontact. 1.0f just takes Sonar, if contact (otherwise baro)
    cfg.snr_diff                  = 0;          // 0 disables that check. Range (0-200) Maximal allowed difference in cm between sonar readouts (100ms rate and snr_diff = 50 means max 5m/s)
    cfg.snr_land                  = 1;          // Aided Sonar - landing, by setting upper throttle limit to current throttle. - Beware of Trees!! Can be disabled for Failsafe with fs_nosnr = 1

    cfg.FDUsedDatasets            = 0;          // Default no Datasets stored
    cfg.stat_clear                = 1;          // This will clear the stats between flights, or you can set to 0 and treasue overallstats, but you have to write manually eeprom or have logging enabled
    cfg.sens_1G                   = 1;          // Just feed a dummy "1" to avoid div by zero
    ClearStats();

    for (i = 0; i < MAX_MOTORS; i++) cfg.customMixer[i].throttle = 0.0f;// custom mixer. clear by Dfaults.
    writeParams(0);
}
예제 #3
0
void checkFirstTime(bool reset)
{
    uint8_t test_val, i;

    test_val = *(uint8_t *) FLASH_WRITE_ADDR;

    if (!reset && test_val == checkNewConf)
        return;

    // Default settings
    cfg.version = checkNewConf;
    cfg.mixerConfiguration = MULTITYPE_QUADX;
    featureClearAll();
    featureSet(FEATURE_VBAT);

    cfg.looptime = 0;
    cfg.P8[ROLL] = 40;
    cfg.I8[ROLL] = 30;
    cfg.D8[ROLL] = 23;
    cfg.P8[PITCH] = 40;
    cfg.I8[PITCH] = 30;
    cfg.D8[PITCH] = 23;
    cfg.P8[YAW] = 85;
    cfg.I8[YAW] = 45;
    cfg.D8[YAW] = 0;
    cfg.P8[PIDALT] = 16;
    cfg.I8[PIDALT] = 15;
    cfg.D8[PIDALT] = 7;
    cfg.P8[PIDPOS] = 11; // POSHOLD_P * 100;
    cfg.I8[PIDPOS] = 0; // POSHOLD_I * 100;
    cfg.D8[PIDPOS] = 0;
    cfg.P8[PIDPOSR] = 20; // POSHOLD_RATE_P * 10;
    cfg.I8[PIDPOSR] = 8; // POSHOLD_RATE_I * 100;
    cfg.D8[PIDPOSR] = 45; // POSHOLD_RATE_D * 1000;
    cfg.P8[PIDNAVR] = 14; // NAV_P * 10;
    cfg.I8[PIDNAVR] = 20; // NAV_I * 100;
    cfg.D8[PIDNAVR] = 80; // NAV_D * 1000;
    cfg.P8[PIDLEVEL] = 70;
    cfg.I8[PIDLEVEL] = 10;
    cfg.D8[PIDLEVEL] = 20;
    cfg.P8[PIDMAG] = 40;
    cfg.P8[PIDVEL] = 0;
    cfg.I8[PIDVEL] = 0;
    cfg.D8[PIDVEL] = 0;
    cfg.rcRate8 = 90;
    cfg.rcExpo8 = 65;
    cfg.rollPitchRate = 0;
    cfg.yawRate = 0;
    cfg.dynThrPID = 0;
    cfg.thrMid8 = 50;
    cfg.thrExpo8 = 0;
    for (i = 0; i < CHECKBOXITEMS; i++)
        cfg.activate[i] = 0;
    cfg.angleTrim[0] = 0;
    cfg.angleTrim[1] = 0;
    cfg.accZero[0] = 0;
    cfg.accZero[1] = 0;
    cfg.accZero[2] = 0;
    cfg.mag_declination = 0;    // For example, -6deg 37min, = -637 Japan, format is [sign]dddmm (degreesminutes) default is zero.
    cfg.acc_hardware = ACC_DEFAULT;     // default/autodetect
    cfg.acc_lpf_factor = 4;
    cfg.acc_lpf_for_velocity = 10;
    cfg.accz_deadband = 50;
    cfg.gyro_cmpf_factor = 400; // default MWC
    cfg.gyro_lpf = 42;
    cfg.mpu6050_scale = 1; // f**k invensense
    cfg.baro_tab_size = 21;
    cfg.baro_noise_lpf = 0.6f;
    cfg.baro_cf = 0.985f;
    cfg.gyro_smoothing_factor = 0x00141403;     // default factors of 20, 20, 3 for R/P/Y
    cfg.vbatscale = 110;
    cfg.vbatmaxcellvoltage = 43;
    cfg.vbatmincellvoltage = 33;

    // Radio
    parseRcChannels("AETR1234");
    cfg.deadband = 0;
    cfg.yawdeadband = 0;
    cfg.alt_hold_throttle_neutral = 20;
    cfg.spektrum_hires = 0;
    cfg.midrc = 1500;
    cfg.mincheck = 1100;
    cfg.maxcheck = 1900;
    cfg.retarded_arm = 0;       // disable arm/disarm on roll left/right

    // Failsafe Variables
    cfg.failsafe_delay = 10;            // 1sec
    cfg.failsafe_off_delay = 200;       // 20sec
    cfg.failsafe_throttle = 1200;       // decent default which should always be below hover throttle for people.

    // Motor/ESC/Servo
    cfg.minthrottle = 1150;
    cfg.maxthrottle = 1850;
    cfg.mincommand = 1000;
    cfg.motor_pwm_rate = 400;
    cfg.servo_pwm_rate = 50;

    // servos
    cfg.yaw_direction = 1;
    cfg.tri_yaw_middle = 1500;
    cfg.tri_yaw_min = 1020;
    cfg.tri_yaw_max = 2000;

    // flying wing
    cfg.wing_left_min = 1020;
    cfg.wing_left_mid = 1500;
    cfg.wing_left_max = 2000;
    cfg.wing_right_min = 1020;
    cfg.wing_right_mid = 1500;
    cfg.wing_right_max = 2000;
    cfg.pitch_direction_l = 1;
    cfg.pitch_direction_r = -1;
    cfg.roll_direction_l = 1;
    cfg.roll_direction_r = 1;

    // gimbal
    cfg.gimbal_pitch_gain = 10;
    cfg.gimbal_roll_gain = 10;
    cfg.gimbal_flags = GIMBAL_NORMAL;
    cfg.gimbal_pitch_min = 1020;
    cfg.gimbal_pitch_max = 2000;
    cfg.gimbal_pitch_mid = 1500;
    cfg.gimbal_roll_min = 1020;
    cfg.gimbal_roll_max = 2000;
    cfg.gimbal_roll_mid = 1500;

    // gps/nav stuff
    cfg.gps_type = GPS_NMEA;
    cfg.gps_baudrate = 115200;
    cfg.gps_wp_radius = 200;
    cfg.gps_lpf = 20;
    cfg.nav_slew_rate = 30;
    cfg.nav_controls_heading = 1;
    cfg.nav_speed_min = 100;
    cfg.nav_speed_max = 300;

    // serial (USART1) baudrate
    cfg.serial_baudrate = 115200;

    // custom mixer. clear by defaults.
    for (i = 0; i < MAX_MOTORS; i++)
        cfg.customMixer[i].throttle = 0.0f;

    writeParams(0);
}
예제 #4
0
파일: serial.c 프로젝트: fiendie/baseflight
static void evaluateCommand(void)
{
    uint32_t i, j, tmp, junk;
#ifdef GPS
    uint8_t wp_no;
    int32_t lat = 0, lon = 0, alt = 0;
#endif
    const char *build = __DATE__;

    switch (currentPortState->cmdMSP) {
        case MSP_SET_RAW_RC:
            for (i = 0; i < 8; i++)
                rcData[i] = read16();
            headSerialReply(0);
            mspFrameRecieve();
            break;
        case MSP_SET_ACC_TRIM:
            cfg.angleTrim[PITCH] = read16();
            cfg.angleTrim[ROLL]  = read16();
            headSerialReply(0);
            break;
#ifdef GPS
        case MSP_SET_RAW_GPS:
            f.GPS_FIX = read8();
            GPS_numSat = read8();
            GPS_coord[LAT] = read32();
            GPS_coord[LON] = read32();
            GPS_altitude = read16();
            GPS_speed = read16();
            GPS_update |= 2;        // New data signalisation to GPS functions
            headSerialReply(0);
            break;
#endif
        case MSP_SET_PID:
            for (i = 0; i < PIDITEMS; i++) {
                cfg.P8[i] = read8();
                cfg.I8[i] = read8();
                cfg.D8[i] = read8();
            }
            headSerialReply(0);
            break;
        case MSP_SET_BOX:
            for (i = 0; i < numberBoxItems; i++)
                cfg.activate[availableBoxes[i]] = read16();
            headSerialReply(0);
            break;
        case MSP_SET_RC_TUNING:
            cfg.rcRate8 = read8();
            cfg.rcExpo8 = read8();
            cfg.rollPitchRate = read8();
            cfg.yawRate = read8();
            cfg.dynThrPID = read8();
            cfg.thrMid8 = read8();
            cfg.thrExpo8 = read8();
            headSerialReply(0);
            break;
        case MSP_SET_MISC:
            tmp = read16();
            // sanity check
            if (tmp < 1600 && tmp > 1400)
                mcfg.midrc = tmp;
            mcfg.minthrottle = read16();
            mcfg.maxthrottle = read16();
            mcfg.mincommand = read16();
            cfg.failsafe_throttle = read16();
            mcfg.gps_type = read8();
            mcfg.gps_baudrate = read8();
            mcfg.gps_ubx_sbas = read8();
            mcfg.multiwiicurrentoutput = read8();
            mcfg.rssi_aux_channel = read8();
            read8();
            cfg.mag_declination = read16() * 10;
            mcfg.vbatscale = read8();           // actual vbatscale as intended
            mcfg.vbatmincellvoltage = read8();  // vbatlevel_warn1 in MWC2.3 GUI
            mcfg.vbatmaxcellvoltage = read8();  // vbatlevel_warn2 in MWC2.3 GUI
            mcfg.vbatwarningcellvoltage = read8(); // vbatlevel when buzzer starts to alert
            headSerialReply(0);
            break;
        case MSP_SET_MOTOR:
            for (i = 0; i < 8; i++)
                motor_disarmed[i] = read16();
            headSerialReply(0);
            break;
        case MSP_SELECT_SETTING:
            if (!f.ARMED) {
                mcfg.current_profile = read8();
                if (mcfg.current_profile > 2)
                    mcfg.current_profile = 0;
                // this writes new profile index and re-reads it
                writeEEPROM(0, false);
            }
            headSerialReply(0);
            break;
        case MSP_SET_HEAD:
            magHold = read16();
            headSerialReply(0);
            break;
        case MSP_IDENT:
            headSerialReply(7);
            serialize8(VERSION);                    // multiwii version
            serialize8(mcfg.mixerConfiguration);    // type of multicopter
            serialize8(MSP_VERSION);                // MultiWii Serial Protocol Version
            serialize32(CAP_PLATFORM_32BIT | CAP_BASEFLIGHT_CONFIG | CAP_DYNBALANCE | CAP_FW_FLAPS); // "capability"
            break;
        case MSP_STATUS:
            headSerialReply(11);
            serialize16(cycleTime);
            serialize16(i2cGetErrorCounter());
            serialize16(sensors(SENSOR_ACC) | sensors(SENSOR_BARO) << 1 | sensors(SENSOR_MAG) << 2 | sensors(SENSOR_GPS) << 3 | sensors(SENSOR_SONAR) << 4);
            // OK, so you waste all the f*****g time to have BOXNAMES and BOXINDEXES etc, and then you go ahead and serialize enabled shit simply by stuffing all
            // the bits in order, instead of setting the enabled bits based on BOXINDEX. WHERE IS THE F*****G LOGIC IN THIS, FUCKWADS.
            // Serialize the boxes in the order we delivered them, until multiwii retards fix their shit
            junk = 0;
            tmp = f.ANGLE_MODE << BOXANGLE | f.HORIZON_MODE << BOXHORIZON |
                  f.BARO_MODE << BOXBARO | f.MAG_MODE << BOXMAG | f.HEADFREE_MODE << BOXHEADFREE | rcOptions[BOXHEADADJ] << BOXHEADADJ |
                  rcOptions[BOXCAMSTAB] << BOXCAMSTAB | rcOptions[BOXCAMTRIG] << BOXCAMTRIG |
                  f.GPS_HOME_MODE << BOXGPSHOME | f.GPS_HOLD_MODE << BOXGPSHOLD |
                  f.PASSTHRU_MODE << BOXPASSTHRU |
                  rcOptions[BOXBEEPERON] << BOXBEEPERON |
                  rcOptions[BOXLEDMAX] << BOXLEDMAX |
                  rcOptions[BOXLLIGHTS] << BOXLLIGHTS |
                  rcOptions[BOXVARIO] << BOXVARIO |
                  rcOptions[BOXCALIB] << BOXCALIB |
                  rcOptions[BOXGOV] << BOXGOV |
                  rcOptions[BOXOSD] << BOXOSD |
                  rcOptions[BOXTELEMETRY] << BOXTELEMETRY |
                  rcOptions[BOXSERVO1] << BOXSERVO1 |
                  rcOptions[BOXSERVO2] << BOXSERVO2 |
                  rcOptions[BOXSERVO3] << BOXSERVO3 |
                  f.ARMED << BOXARM;
            for (i = 0; i < numberBoxItems; i++) {
                int flag = (tmp & (1 << availableBoxes[i]));
                if (flag)
                    junk |= 1 << i;
            }
            serialize32(junk);
            serialize8(mcfg.current_profile);
            break;
        case MSP_RAW_IMU:
            headSerialReply(18);
            // Retarded hack until multiwiidorks start using real units for sensor data
            if (acc_1G > 1024) {
                for (i = 0; i < 3; i++)
                    serialize16(accSmooth[i] / 8);
            } else {
                for (i = 0; i < 3; i++)
                    serialize16(accSmooth[i]);
            }
            for (i = 0; i < 3; i++)
                serialize16(gyroData[i]);
            for (i = 0; i < 3; i++)
                serialize16(magADC[i]);
            break;
        case MSP_SERVO:
            s_struct((uint8_t *)&servo, 16);
            break;
        case MSP_SERVO_CONF:
            headSerialReply(56);
            for (i = 0; i < MAX_SERVOS; i++) {
                serialize16(cfg.servoConf[i].min);
                serialize16(cfg.servoConf[i].max);
                serialize16(cfg.servoConf[i].middle);
                serialize8(getOldServoConfig(i));
            }
            break;
        case MSP_SET_SERVO_CONF:
            headSerialReply(0);
            for (i = 0; i < MAX_SERVOS; i++) {
                cfg.servoConf[i].min = read16();
                cfg.servoConf[i].max = read16();
                cfg.servoConf[i].middle = read16();
                tmp = read8();
                // trash old servo direction
                cfg.servoConf[i].rate = tmp & 0xfc;

                // store old style servo direction depending on current mixer configuration
                switch (mcfg.mixerConfiguration) {
                    case MULTITYPE_BI:
                        storeOldServoConfig(i, tmp, 4, 1, INPUT_PITCH);
                        storeOldServoConfig(i, tmp, 5, 1, INPUT_PITCH);

                        storeOldServoConfig(i, tmp, 4, 2, INPUT_YAW);
                        storeOldServoConfig(i, tmp, 5, 2, INPUT_YAW);

                        break;
                    case MULTITYPE_TRI:
                        storeOldServoConfig(i, tmp, 5, 1, INPUT_YAW);

                        break;
                    case MULTITYPE_FLYING_WING:
                        storeOldServoConfig(i, tmp, 3, 1, INPUT_PITCH);
                        storeOldServoConfig(i, tmp, 4, 1, INPUT_PITCH);

                        storeOldServoConfig(i, tmp, 3, 2, INPUT_ROLL);
                        storeOldServoConfig(i, tmp, 4, 2, INPUT_ROLL);

                        break;
                    case MULTITYPE_DUALCOPTER:
                        storeOldServoConfig(i, tmp, 4, 1, INPUT_PITCH);
                        storeOldServoConfig(i, tmp, 5, 1, INPUT_ROLL);

                        break;
                    case MULTITYPE_SINGLECOPTER:
                        storeOldServoConfig(i, tmp, 3, 1, INPUT_PITCH);
                        storeOldServoConfig(i, tmp, 4, 1, INPUT_PITCH);
                        storeOldServoConfig(i, tmp, 5, 1, INPUT_ROLL);
                        storeOldServoConfig(i, tmp, 6, 1, INPUT_ROLL);

                        storeOldServoConfig(i, tmp, 3, 2, INPUT_YAW);
                        storeOldServoConfig(i, tmp, 4, 2, INPUT_YAW);
                        storeOldServoConfig(i, tmp, 5, 2, INPUT_YAW);
                        storeOldServoConfig(i, tmp, 6, 2, INPUT_YAW);

                        break;
                }
            }
            break;
        case MSP_MOTOR:
            s_struct((uint8_t *)motor, 16);
            break;
        case MSP_RC:
            headSerialReply(16);
            for (i = 0; i < 8; i++)
                serialize16(rcData[i]);
            break;
#ifdef GPS
        case MSP_RAW_GPS:
            headSerialReply(16);
            serialize8(f.GPS_FIX);
            serialize8(GPS_numSat);
            serialize32(GPS_coord[LAT]);
            serialize32(GPS_coord[LON]);
            serialize16(GPS_altitude);
            serialize16(GPS_speed);
            serialize16(GPS_ground_course);
            break;
        case MSP_COMP_GPS:
            headSerialReply(5);
            serialize16(GPS_distanceToHome);
            serialize16(GPS_directionToHome);
            serialize8(GPS_update & 1);
            break;
#endif
        case MSP_ATTITUDE:
            headSerialReply(6);
            for (i = 0; i < 2; i++)
                serialize16(angle[i]);
            serialize16(heading);
            break;
        case MSP_ALTITUDE:
            headSerialReply(6);
            serialize32(EstAlt);
            serialize16(vario);
            break;
        case MSP_ANALOG:
            headSerialReply(7);
            serialize8((uint8_t)constrain(vbat, 0, 255));
            serialize16((uint16_t)constrain(mAhdrawn, 0, 0xFFFF)); // milliamphours drawn from battery
            serialize16(rssi);
            if (mcfg.multiwiicurrentoutput)
                serialize16((uint16_t)constrain((abs(amperage) * 10), 0, 0xFFFF)); // send amperage in 0.001 A steps
            else
                serialize16((uint16_t)constrain(abs(amperage), 0, 0xFFFF)); // send amperage in 0.01 A steps
            break;
        case MSP_RC_TUNING:
            headSerialReply(7);
            serialize8(cfg.rcRate8);
            serialize8(cfg.rcExpo8);
            serialize8(cfg.rollPitchRate);
            serialize8(cfg.yawRate);
            serialize8(cfg.dynThrPID);
            serialize8(cfg.thrMid8);
            serialize8(cfg.thrExpo8);
            break;
        case MSP_PID:
            headSerialReply(3 * PIDITEMS);
            for (i = 0; i < PIDITEMS; i++) {
                serialize8(cfg.P8[i]);
                serialize8(cfg.I8[i]);
                serialize8(cfg.D8[i]);
            }
            break;
        case MSP_PIDNAMES:
            headSerialReply(sizeof(pidnames) - 1);
            serializeNames(pidnames);
            break;
        case MSP_BOX:
            headSerialReply(2 * numberBoxItems);
            for (i = 0; i < numberBoxItems; i++)
                serialize16(cfg.activate[availableBoxes[i]]);
            break;
        case MSP_BOXNAMES:
            // headSerialReply(sizeof(boxnames) - 1);
            serializeBoxNamesReply();
            break;
        case MSP_BOXIDS:
            headSerialReply(numberBoxItems);
            for (i = 0; i < numberBoxItems; i++) {
                for  (j = 0; j < CHECKBOXITEMS; j++) {
                    if (boxes[j].permanentId == availableBoxes[i])
                        serialize8(boxes[j].permanentId);
                }
            }
            break;
        case MSP_MISC:
            headSerialReply(2 * 6 + 4 + 2 + 4);
            serialize16(mcfg.midrc);
            serialize16(mcfg.minthrottle);
            serialize16(mcfg.maxthrottle);
            serialize16(mcfg.mincommand);
            serialize16(cfg.failsafe_throttle);
            serialize8(mcfg.gps_type);
            serialize8(mcfg.gps_baudrate);
            serialize8(mcfg.gps_ubx_sbas);
            serialize8(mcfg.multiwiicurrentoutput);
            serialize8(mcfg.rssi_aux_channel);
            serialize8(0);
            serialize16(cfg.mag_declination / 10); // TODO check this shit
            serialize8(mcfg.vbatscale);
            serialize8(mcfg.vbatmincellvoltage);
            serialize8(mcfg.vbatmaxcellvoltage);
            serialize8(mcfg.vbatwarningcellvoltage);
            break;
        case MSP_MOTOR_PINS:
            headSerialReply(8);
            for (i = 0; i < 8; i++)
                serialize8(i + 1);
            break;
#ifdef GPS
        case MSP_WP:
            wp_no = read8();    // get the wp number
            headSerialReply(18);
            if (wp_no == 0) {
                lat = GPS_home[LAT];
                lon = GPS_home[LON];
            } else if (wp_no == 16) {
                lat = GPS_hold[LAT];
                lon = GPS_hold[LON];
            }
            serialize8(wp_no);
            serialize32(lat);
            serialize32(lon);
            serialize32(AltHold);           // altitude (cm) will come here -- temporary implementation to test feature with apps
            serialize16(0);                 // heading  will come here (deg)
            serialize16(0);                 // time to stay (ms) will come here
            serialize8(0);                  // nav flag will come here
            break;
        case MSP_SET_WP:
            wp_no = read8();    //get the wp number
            lat = read32();
            lon = read32();
            alt = read32();     // to set altitude (cm)
            read16();           // future: to set heading (deg)
            read16();           // future: to set time to stay (ms)
            read8();            // future: to set nav flag
            if (wp_no == 0) {
                GPS_home[LAT] = lat;
                GPS_home[LON] = lon;
                f.GPS_HOME_MODE = 0;        // with this flag, GPS_set_next_wp will be called in the next loop -- OK with SERIAL GPS / OK with I2C GPS
                f.GPS_FIX_HOME = 1;
                if (alt != 0)
                    AltHold = alt;          // temporary implementation to test feature with apps
            } else if (wp_no == 16) {       // OK with SERIAL GPS  --  NOK for I2C GPS / needs more code dev in order to inject GPS coord inside I2C GPS
                GPS_hold[LAT] = lat;
                GPS_hold[LON] = lon;
                if (alt != 0)
                    AltHold = alt;          // temporary implementation to test feature with apps
                nav_mode = NAV_MODE_WP;
                GPS_set_next_wp(&GPS_hold[LAT], &GPS_hold[LON]);
            }
            headSerialReply(0);
            break;
#endif /* GPS */
        case MSP_RESET_CONF:
            if (!f.ARMED)
                checkFirstTime(true);
            headSerialReply(0);
            break;
        case MSP_ACC_CALIBRATION:
            if (!f.ARMED)
                calibratingA = CALIBRATING_ACC_CYCLES;
            headSerialReply(0);
            break;
        case MSP_MAG_CALIBRATION:
            if (!f.ARMED)
                f.CALIBRATE_MAG = 1;
            headSerialReply(0);
            break;
        case MSP_EEPROM_WRITE:
            if (f.ARMED) {
                headSerialError(0);
            } else {
                writeEEPROM(0, true);
                headSerialReply(0);
            }
            break;
        case MSP_DEBUG:
            headSerialReply(8);
            // make use of this crap, output some useful QA statistics
            debug[3] = ((hse_value / 1000000) * 1000) + (SystemCoreClock / 1000000);         // XX0YY [crystal clock : core clock]
            for (i = 0; i < 4; i++)
                serialize16(debug[i]);      // 4 variables are here for general monitoring purpose
            break;

        // Additional commands that are not compatible with MultiWii
        case MSP_ACC_TRIM:
            headSerialReply(4);
            serialize16(cfg.angleTrim[PITCH]);
            serialize16(cfg.angleTrim[ROLL]);
            break;
        case MSP_UID:
            headSerialReply(12);
            serialize32(U_ID_0);
            serialize32(U_ID_1);
            serialize32(U_ID_2);
            break;
#ifdef GPS
        case MSP_GPSSVINFO:
            headSerialReply(1 + (GPS_numCh * 4));
            serialize8(GPS_numCh);
            for (i = 0; i < GPS_numCh; i++) {
                serialize8(GPS_svinfo_chn[i]);
                serialize8(GPS_svinfo_svid[i]);
                serialize8(GPS_svinfo_quality[i]);
                serialize8(GPS_svinfo_cno[i]);
            }
            // Poll new SVINFO from GPS
            gpsPollSvinfo();
            break;
        case MSP_GPSDEBUGINFO:
            headSerialReply(16);
            if (sensors(SENSOR_GPS)) {
                serialize32(GPS_update_rate[1] - GPS_update_rate[0]);
                serialize32(GPS_svinfo_rate[1] - GPS_svinfo_rate[0]);
            } else {
                serialize32(0);
                serialize32(0);
            }
            serialize32(GPS_HorizontalAcc);
            serialize32(GPS_VerticalAcc);
            break;
#endif /* GPS */

        case MSP_SET_CONFIG:
            headSerialReply(0);
            mcfg.mixerConfiguration = read8(); // multitype
            featureClearAll();
            featureSet(read32()); // features bitmap
            mcfg.serialrx_type = read8(); // serialrx_type
            mcfg.board_align_roll = read16(); // board_align_roll
            mcfg.board_align_pitch = read16(); // board_align_pitch
            mcfg.board_align_yaw = read16(); // board_align_yaw
            mcfg.currentscale = read16();
            mcfg.currentoffset = read16();
            /// ???
            break;
        case MSP_CONFIG:
            headSerialReply(1 + 4 + 1 + 2 + 2 + 2 + 4);
            serialize8(mcfg.mixerConfiguration);
            serialize32(featureMask());
            serialize8(mcfg.serialrx_type);
            serialize16(mcfg.board_align_roll);
            serialize16(mcfg.board_align_pitch);
            serialize16(mcfg.board_align_yaw);
            serialize16(mcfg.currentscale);
            serialize16(mcfg.currentoffset);
            /// ???
            break;

        case MSP_RCMAP:
            headSerialReply(MAX_INPUTS); // TODO fix this
            for (i = 0; i < MAX_INPUTS; i++)
                serialize8(mcfg.rcmap[i]);
            break;
        case MSP_SET_RCMAP:
            headSerialReply(0);
            for (i = 0; i < MAX_INPUTS; i++)
                mcfg.rcmap[i] = read8();
            break;

        case MSP_REBOOT:
            headSerialReply(0);
            pendReboot = true;
            break;

        case MSP_BUILDINFO:
            headSerialReply(11 + 4 + 4);
            for (i = 0; i < 11; i++)
                serialize8(build[i]); // MMM DD YYYY as ascii, MMM = Jan/Feb... etc
            serialize32(0); // future exp
            serialize32(0); // future exp
            break;

        default:                   // we do not know how to handle the (valid) message, indicate error MSP $M!
            headSerialError(0);
            break;
    }
    tailSerialReply();
}
예제 #5
0
// Default settings
static void resetConf(void)
{
    int i;
    const int8_t default_align[3][3] = { /* GYRO */ { 0, 0, 0 }, /* ACC */ { 0, 0, 0 }, /* MAG */ { -2, -3, 1 } };

    // Clear all configuration
    memset(&mcfg, 0, sizeof(master_t));
    memset(&cfg, 0, sizeof(config_t));

    mcfg.version = EEPROM_CONF_VERSION;
    mcfg.mixerConfiguration = MULTITYPE_QUADX;
    featureClearAll();
    featureSet(FEATURE_VBAT);
		featureSet(FEATURE_PPM);

    // global settings
    mcfg.current_profile = 0;       // default profile
    mcfg.gyro_cmpf_factor = 600;    // default MWC
    mcfg.gyro_cmpfm_factor = 250;   // default MWC
    mcfg.gyro_lpf = 20;             // supported by all gyro drivers now. In case of ST gyro, will default to 32Hz instead
    mcfg.accZero[0] = 0;
    mcfg.accZero[1] = 0;
    mcfg.accZero[2] = 0;
    memcpy(&mcfg.align, default_align, sizeof(mcfg.align));
    mcfg.acc_hardware = ACC_DEFAULT;     // default/autodetect
    mcfg.moron_threshold = 32;
    mcfg.gyro_smoothing_factor = 0x00141403;     // default factors of 20, 20, 3 for R/P/Y
    mcfg.vbatscale = 110;
    mcfg.vbatmaxcellvoltage = 43;
    mcfg.vbatmincellvoltage = 33;
    mcfg.power_adc_channel = 0;
    mcfg.spektrum_hires = 0;
    mcfg.midrc = 1500;
    mcfg.mincheck = 1100;
    mcfg.maxcheck = 1900;
    mcfg.retarded_arm = 0;       // disable arm/disarm on roll left/right
    // Motor/ESC/Servo
    mcfg.minthrottle = 1250;
    mcfg.maxthrottle = 1850;
    mcfg.mincommand = 1000;
    mcfg.motor_pwm_rate = 400;
    mcfg.servo_pwm_rate = 50;
    // gps/nav stuff
    mcfg.gps_type = GPS_NMEA;
    mcfg.gps_baudrate = 115200;
    // serial (USART1) baudrate
    mcfg.serial_baudrate = 115200;
    mcfg.looptime = 3000;
    cfg.pidController = 0;
    cfg.P8[ROLL] = 40;
    cfg.I8[ROLL] = 30;
    cfg.D8[ROLL] = 23;
    cfg.P8[PITCH] = 40;
    cfg.I8[PITCH] = 30;
    cfg.D8[PITCH] = 23;
    cfg.P8[YAW] = 85;
    cfg.I8[YAW] = 45;
    cfg.D8[YAW] = 0;
    cfg.P8[PIDALT] = 64;
    cfg.I8[PIDALT] = 25;
    cfg.D8[PIDALT] = 24;
    cfg.P8[PIDPOS] = 11; // POSHOLD_P * 100;
    cfg.I8[PIDPOS] = 0; // POSHOLD_I * 100;
    cfg.D8[PIDPOS] = 0;
    cfg.P8[PIDPOSR] = 20; // POSHOLD_RATE_P * 10;
    cfg.I8[PIDPOSR] = 8; // POSHOLD_RATE_I * 100;
    cfg.D8[PIDPOSR] = 45; // POSHOLD_RATE_D * 1000;
    cfg.P8[PIDNAVR] = 14; // NAV_P * 10;
    cfg.I8[PIDNAVR] = 20; // NAV_I * 100;
    cfg.D8[PIDNAVR] = 80; // NAV_D * 1000;
    cfg.P8[PIDLEVEL] = 90;
    cfg.I8[PIDLEVEL] = 10;
    cfg.D8[PIDLEVEL] = 100;
    cfg.P8[PIDMAG] = 40;
    cfg.P8[PIDVEL] = 0;
    cfg.I8[PIDVEL] = 0;
    cfg.D8[PIDVEL] = 0;
    cfg.rcRate8 = 90;
    cfg.rcExpo8 = 65;
    cfg.rollPitchRate = 0;
    cfg.yawRate = 0;
    cfg.dynThrPID = 0;
    cfg.thrMid8 = 50;
    cfg.thrExpo8 = 0;
    // for (i = 0; i < CHECKBOXITEMS; i++)
    //     cfg.activate[i] = 0;
    cfg.angleTrim[0] = 0;
    cfg.angleTrim[1] = 0;
    cfg.mag_declination = 625;    // For example, -6deg 37min, = -637 Japan, format is [sign]dddmm (degreesminutes) default is zero.
    cfg.acc_lpf_factor = 20;
    cfg.accz_deadband = 10;
    cfg.baro_tab_size = 21;
    cfg.baro_noise_lpf = 0.6f;
    cfg.baro_cf = 0.985f;

    // Radio
    parseRcChannels("AETR1234");
    cfg.deadband = 20;
    cfg.yawdeadband = 20;
    cfg.alt_hold_throttle_neutral = 40;
    cfg.alt_hold_fast_change = 1;

    // Failsafe Variables
    cfg.failsafe_delay = 10;                // 1sec
    cfg.failsafe_off_delay = 200;           // 20sec
    cfg.failsafe_throttle = 1200;           // decent default which should always be below hover throttle for people.
    cfg.failsafe_detect_threshold = 985;    // any of first 4 channels below this value will trigger failsafe

    // servos
    cfg.yaw_direction = 1;
    cfg.tri_yaw_middle = 1500;
    cfg.tri_yaw_min = 1020;
    cfg.tri_yaw_max = 2000;

    // flying wing
    cfg.wing_left_min = 1020;
    cfg.wing_left_mid = 1500;
    cfg.wing_left_max = 2000;
    cfg.wing_right_min = 1020;
    cfg.wing_right_mid = 1500;
    cfg.wing_right_max = 2000;
    cfg.pitch_direction_l = 1;
    cfg.pitch_direction_r = -1;
    cfg.roll_direction_l = 1;
    cfg.roll_direction_r = 1;

    // gimbal
    cfg.gimbal_pitch_gain = 10;
    cfg.gimbal_roll_gain = 10;
    cfg.gimbal_flags = GIMBAL_NORMAL;
    cfg.gimbal_pitch_min = 1020;
    cfg.gimbal_pitch_max = 2000;
    cfg.gimbal_pitch_mid = 1500;
    cfg.gimbal_roll_min = 1020;
    cfg.gimbal_roll_max = 2000;
    cfg.gimbal_roll_mid = 1500;

    // gps/nav stuff
    cfg.gps_wp_radius = 200;
    cfg.gps_lpf = 20;
    cfg.nav_slew_rate = 30;
    cfg.nav_controls_heading = 1;
    cfg.nav_speed_min = 100;
    cfg.nav_speed_max = 300;
    cfg.ap_mode = 40;

    // custom mixer. clear by defaults.
    for (i = 0; i < MAX_MOTORS; i++)
        mcfg.customMixer[i].throttle = 0.0f;

    // copy default config into all 3 profiles
    for (i = 0; i < 3; i++)
        memcpy(&mcfg.profile[i], &cfg, sizeof(config_t));
}
예제 #6
0
// Default settings
static void resetConf(void)
{
    int i;
    int8_t servoRates[8] = { 30, 30, 100, 100, 100, 100, 100, 100 };

    // Clear all configuration
    memset(&masterConfig, 0, sizeof(master_t));
    setProfile(0);
    setControlRateProfile(0);

    masterConfig.version = EEPROM_CONF_VERSION;
    masterConfig.mixerConfiguration = MULTITYPE_QUADX;
    featureClearAll();
#if defined(CJMCU) || defined(SPARKY)
    featureSet(FEATURE_RX_PPM);
#endif
    featureSet(FEATURE_VBAT);

    // global settings
    masterConfig.current_profile_index = 0;     // default profile
    masterConfig.gyro_cmpf_factor = 600;        // default MWC
    masterConfig.gyro_cmpfm_factor = 250;       // default MWC
    masterConfig.gyro_lpf = 42;                 // supported by all gyro drivers now. In case of ST gyro, will default to 32Hz instead

    resetAccelerometerTrims(&masterConfig.accZero);

    resetSensorAlignment(&masterConfig.sensorAlignmentConfig);

    masterConfig.boardAlignment.rollDegrees = 0;
    masterConfig.boardAlignment.pitchDegrees = 0;
    masterConfig.boardAlignment.yawDegrees = 0;
    masterConfig.acc_hardware = ACC_DEFAULT;     // default/autodetect
    masterConfig.max_angle_inclination = 500;    // 50 degrees
    masterConfig.yaw_control_direction = 1;
    masterConfig.gyroConfig.gyroMovementCalibrationThreshold = 32;

    resetBatteryConfig(&masterConfig.batteryConfig);

    resetTelemetryConfig(&masterConfig.telemetryConfig);

    masterConfig.rxConfig.serialrx_provider = 0;
    masterConfig.rxConfig.spektrum_sat_bind = 0;
    masterConfig.rxConfig.midrc = 1500;
    masterConfig.rxConfig.mincheck = 1100;
    masterConfig.rxConfig.maxcheck = 1900;
    masterConfig.rxConfig.rssi_channel = 0;
    masterConfig.rxConfig.rssi_scale = RSSI_SCALE_DEFAULT;

    masterConfig.inputFilteringMode = INPUT_FILTERING_DISABLED;

    masterConfig.retarded_arm = 0;
    masterConfig.disarm_kill_switch = 1;
    masterConfig.small_angle = 25;

    masterConfig.airplaneConfig.flaps_speed = 0;
    masterConfig.airplaneConfig.fixedwing_althold_dir = 1;

    // Motor/ESC/Servo
    resetEscAndServoConfig(&masterConfig.escAndServoConfig);
    resetFlight3DConfig(&masterConfig.flight3DConfig);

#ifdef BRUSHED_MOTORS
    masterConfig.motor_pwm_rate = BRUSHED_MOTORS_PWM_RATE;
#else
    masterConfig.motor_pwm_rate = BRUSHLESS_MOTORS_PWM_RATE;
#endif
    masterConfig.servo_pwm_rate = 50;

#ifdef GPS
    // gps/nav stuff
    masterConfig.gpsConfig.provider = GPS_NMEA;
    masterConfig.gpsConfig.sbasMode = SBAS_AUTO;
    masterConfig.gpsConfig.autoConfig = GPS_AUTOCONFIG_ON;
    masterConfig.gpsConfig.autoBaud = GPS_AUTOBAUD_OFF;
#endif

    resetSerialConfig(&masterConfig.serialConfig);

    masterConfig.looptime = 3500;
    masterConfig.emf_avoidance = 0;

    currentProfile->pidController = 0;
    resetPidProfile(&currentProfile->pidProfile);

    resetControlRateConfig(&masterConfig.controlRateProfiles[0]);

    // for (i = 0; i < CHECKBOXITEMS; i++)
    //     cfg.activate[i] = 0;

    resetRollAndPitchTrims(&currentProfile->accelerometerTrims);

    currentProfile->mag_declination = 0;
    currentProfile->acc_lpf_factor = 4;
    currentProfile->accz_lpf_cutoff = 5.0f;
    currentProfile->accDeadband.xy = 40;
    currentProfile->accDeadband.z = 40;

    resetBarometerConfig(&currentProfile->barometerConfig);

    currentProfile->acc_unarmedcal = 1;

    // Radio
    parseRcChannels("AETR1234", &masterConfig.rxConfig);

    resetRcControlsConfig(&currentProfile->rcControlsConfig);

    currentProfile->throttle_correction_value = 0;      // could 10 with althold or 40 for fpv
    currentProfile->throttle_correction_angle = 800;    // could be 80.0 deg with atlhold or 45.0 for fpv

    // Failsafe Variables
    currentProfile->failsafeConfig.failsafe_delay = 10;              // 1sec
    currentProfile->failsafeConfig.failsafe_off_delay = 200;         // 20sec
    currentProfile->failsafeConfig.failsafe_throttle = 1200;         // decent default which should always be below hover throttle for people.
    currentProfile->failsafeConfig.failsafe_min_usec = 985;          // any of first 4 channels below this value will trigger failsafe
    currentProfile->failsafeConfig.failsafe_max_usec = 2115;         // any of first 4 channels above this value will trigger failsafe

    // servos
    for (i = 0; i < 8; i++) {
        currentProfile->servoConf[i].min = DEFAULT_SERVO_MIN;
        currentProfile->servoConf[i].max = DEFAULT_SERVO_MAX;
        currentProfile->servoConf[i].middle = DEFAULT_SERVO_MIDDLE;
        currentProfile->servoConf[i].rate = servoRates[i];
        currentProfile->servoConf[i].forwardFromChannel = CHANNEL_FORWARDING_DISABLED;
    }

    currentProfile->mixerConfig.yaw_direction = 1;
    currentProfile->mixerConfig.tri_unarmed_servo = 1;

    // gimbal
    currentProfile->gimbalConfig.gimbal_flags = GIMBAL_NORMAL;

#ifdef GPS
    resetGpsProfile(&currentProfile->gpsProfile);
#endif

    // custom mixer. clear by defaults.
    for (i = 0; i < MAX_SUPPORTED_MOTORS; i++)
        masterConfig.customMixer[i].throttle = 0.0f;

#ifdef LED_STRIP
    applyDefaultColors(masterConfig.colors, CONFIGURABLE_COLOR_COUNT);
    applyDefaultLedStripConfig(masterConfig.ledConfigs);
#endif

    // copy first profile into remaining profile
    for (i = 1; i < MAX_PROFILE_COUNT; i++) {
        memcpy(&masterConfig.profile[i], currentProfile, sizeof(profile_t));
    }

    // copy first control rate config into remaining profile
    for (i = 1; i < MAX_CONTROL_RATE_PROFILE_COUNT; i++) {
        memcpy(&masterConfig.controlRateProfiles[i], currentControlRateProfile, sizeof(controlRateConfig_t));
    }

    for (i = 1; i < MAX_PROFILE_COUNT; i++) {
        masterConfig.profile[i].defaultRateProfileIndex = i % MAX_CONTROL_RATE_PROFILE_COUNT;
    }
}
예제 #7
0
파일: config.c 프로젝트: gurkenfolie/inav
// Default settings
static void resetConf(void)
{
    int i;

    // Clear all configuration
    memset(&masterConfig, 0, sizeof(master_t));
    setProfile(0);
    setControlRateProfile(0);

    masterConfig.version = EEPROM_CONF_VERSION;
    masterConfig.mixerMode = MIXER_QUADX;
    featureClearAll();
    persistentFlagClearAll();
    featureSet(DEFAULT_RX_FEATURE | FEATURE_FAILSAFE);
#ifdef DEFAULT_FEATURES
    featureSet(DEFAULT_FEATURES);
#endif

#ifdef BOARD_HAS_VOLTAGE_DIVIDER
    // only enable the VBAT feature by default if the board has a voltage divider otherwise
    // the user may see incorrect readings and unexpected issues with pin mappings may occur.
    featureSet(FEATURE_VBAT);
#endif

    // global settings
    masterConfig.current_profile_index = 0;     // default profile
    masterConfig.dcm_kp_acc = 2500;             // 0.25 * 10000
    masterConfig.dcm_ki_acc = 50;               // 0.005 * 10000
    masterConfig.dcm_kp_mag = 10000;            // 1.00 * 10000
    masterConfig.dcm_ki_mag = 0;                // 0.00 * 10000
    masterConfig.gyro_lpf = 3;                  // INV_FILTER_42HZ, In case of ST gyro, will default to 32Hz instead

    resetAccelerometerTrims(&masterConfig.accZero, &masterConfig.accGain);

    resetSensorAlignment(&masterConfig.sensorAlignmentConfig);

    masterConfig.boardAlignment.rollDeciDegrees = 0;
    masterConfig.boardAlignment.pitchDeciDegrees = 0;
    masterConfig.boardAlignment.yawDeciDegrees = 0;
    masterConfig.acc_hardware = ACC_DEFAULT;     // default/autodetect
    masterConfig.gyroConfig.gyroMovementCalibrationThreshold = 32;

    masterConfig.mag_hardware = MAG_DEFAULT;     // default/autodetect
    masterConfig.baro_hardware = BARO_DEFAULT;   // default/autodetect

    resetBatteryConfig(&masterConfig.batteryConfig);

    resetTelemetryConfig(&masterConfig.telemetryConfig);

    masterConfig.rxConfig.serialrx_provider = 0;
    masterConfig.rxConfig.spektrum_sat_bind = 0;
    masterConfig.rxConfig.midrc = 1500;
    masterConfig.rxConfig.mincheck = 1100;
    masterConfig.rxConfig.maxcheck = 1900;
    masterConfig.rxConfig.rx_min_usec = 885;          // any of first 4 channels below this value will trigger rx loss detection
    masterConfig.rxConfig.rx_max_usec = 2115;         // any of first 4 channels above this value will trigger rx loss detection

    for (i = 0; i < MAX_SUPPORTED_RC_CHANNEL_COUNT; i++) {
        rxFailsafeChannelConfiguration_t *channelFailsafeConfiguration = &masterConfig.rxConfig.failsafe_channel_configurations[i];
        channelFailsafeConfiguration->mode = (i < NON_AUX_CHANNEL_COUNT) ? RX_FAILSAFE_MODE_AUTO : RX_FAILSAFE_MODE_HOLD;
        channelFailsafeConfiguration->step = (i == THROTTLE) ? CHANNEL_VALUE_TO_RXFAIL_STEP(masterConfig.rxConfig.rx_min_usec) : CHANNEL_VALUE_TO_RXFAIL_STEP(masterConfig.rxConfig.midrc);
    }

    masterConfig.rxConfig.rssi_channel = 0;
    masterConfig.rxConfig.rssi_scale = RSSI_SCALE_DEFAULT;
    masterConfig.rxConfig.rssi_ppm_invert = 0;
    masterConfig.rxConfig.rcSmoothing = 1;

    resetAllRxChannelRangeConfigurations(masterConfig.rxConfig.channelRanges);

    masterConfig.inputFilteringMode = INPUT_FILTERING_DISABLED;

    masterConfig.disarm_kill_switch = 1;
    masterConfig.auto_disarm_delay = 5;
    masterConfig.small_angle = 25;

    resetMixerConfig(&masterConfig.mixerConfig);

    // Motor/ESC/Servo
    resetEscAndServoConfig(&masterConfig.escAndServoConfig);
    resetFlight3DConfig(&masterConfig.flight3DConfig);

#ifdef BRUSHED_MOTORS
    masterConfig.motor_pwm_rate = BRUSHED_MOTORS_PWM_RATE;
#else
    masterConfig.motor_pwm_rate = BRUSHLESS_MOTORS_PWM_RATE;
#endif
    masterConfig.servo_pwm_rate = 50;

#ifdef GPS
    // gps/nav stuff
    masterConfig.gpsConfig.provider = GPS_UBLOX;
    masterConfig.gpsConfig.sbasMode = SBAS_AUTO;
    masterConfig.gpsConfig.autoConfig = GPS_AUTOCONFIG_ON;
    masterConfig.gpsConfig.autoBaud = GPS_AUTOBAUD_ON;
    masterConfig.gpsConfig.dynModel = GPS_DYNMODEL_AIR_1G;
#endif

#ifdef NAV
    resetNavConfig(&masterConfig.navConfig);
#endif

    resetSerialConfig(&masterConfig.serialConfig);

    masterConfig.looptime = 2000;
    masterConfig.emf_avoidance = 0;
    masterConfig.i2c_overclock = 0;
    masterConfig.gyroSync = 0;
    masterConfig.gyroSyncDenominator = 2;

    resetPidProfile(&currentProfile->pidProfile);

    resetControlRateConfig(&masterConfig.controlRateProfiles[0]);

    // for (i = 0; i < CHECKBOXITEMS; i++)
    //     cfg.activate[i] = 0;

    currentProfile->mag_declination = 0;

    resetBarometerConfig(&masterConfig.barometerConfig);

    // Radio
    parseRcChannels("AETR1234", &masterConfig.rxConfig);

    resetRcControlsConfig(&currentProfile->rcControlsConfig);

    currentProfile->throttle_tilt_compensation_strength = 0;      // 0-100, 0 - disabled

    // Failsafe Variables
    masterConfig.failsafeConfig.failsafe_delay = 10;              // 1sec
    masterConfig.failsafeConfig.failsafe_off_delay = 200;         // 20sec
    masterConfig.failsafeConfig.failsafe_throttle = 1000;         // default throttle off.
    masterConfig.failsafeConfig.failsafe_kill_switch = 0;         // default failsafe switch action is identical to rc link loss
    masterConfig.failsafeConfig.failsafe_throttle_low_delay = 100; // default throttle low delay for "just disarm" on failsafe condition
    masterConfig.failsafeConfig.failsafe_procedure = 0;           // default full failsafe procedure is 0: auto-landing

#ifdef USE_SERVOS
    // servos
    for (i = 0; i < MAX_SUPPORTED_SERVOS; i++) {
        currentProfile->servoConf[i].min = DEFAULT_SERVO_MIN;
        currentProfile->servoConf[i].max = DEFAULT_SERVO_MAX;
        currentProfile->servoConf[i].middle = DEFAULT_SERVO_MIDDLE;
        currentProfile->servoConf[i].rate = 100;
        currentProfile->servoConf[i].angleAtMin = DEFAULT_SERVO_MIN_ANGLE;
        currentProfile->servoConf[i].angleAtMax = DEFAULT_SERVO_MAX_ANGLE;
        currentProfile->servoConf[i].forwardFromChannel = CHANNEL_FORWARDING_DISABLED;
    }

    // gimbal
    currentProfile->gimbalConfig.mode = GIMBAL_MODE_NORMAL;
#endif

    // custom mixer. clear by defaults.
    for (i = 0; i < MAX_SUPPORTED_MOTORS; i++)
        masterConfig.customMotorMixer[i].throttle = 0.0f;

#ifdef LED_STRIP
    applyDefaultColors(masterConfig.colors, CONFIGURABLE_COLOR_COUNT);
    applyDefaultLedStripConfig(masterConfig.ledConfigs);
#endif

#ifdef BLACKBOX
#ifdef ENABLE_BLACKBOX_LOGGING_ON_SPIFLASH_BY_DEFAULT
    featureSet(FEATURE_BLACKBOX);
    masterConfig.blackbox_device = BLACKBOX_DEVICE_FLASH;
#else
    masterConfig.blackbox_device = BLACKBOX_DEVICE_SERIAL;
#endif
    masterConfig.blackbox_rate_num = 1;
    masterConfig.blackbox_rate_denom = 1;
#endif

    // alternative defaults settings for COLIBRI RACE targets
#if defined(COLIBRI_RACE)
    masterConfig.looptime = 1000;

    masterConfig.rxConfig.rcmap[0] = 1;
    masterConfig.rxConfig.rcmap[1] = 2;
    masterConfig.rxConfig.rcmap[2] = 3;
    masterConfig.rxConfig.rcmap[3] = 0;
    masterConfig.rxConfig.rcmap[4] = 4;
    masterConfig.rxConfig.rcmap[5] = 5;
    masterConfig.rxConfig.rcmap[6] = 6;
    masterConfig.rxConfig.rcmap[7] = 7;

    featureSet(FEATURE_ONESHOT125);
    featureSet(FEATURE_VBAT);
    featureSet(FEATURE_LED_STRIP);
    featureSet(FEATURE_FAILSAFE);
#endif

    // alternative defaults settings for ALIENWIIF1 and ALIENWIIF3 targets
#ifdef ALIENWII32
#ifdef ALIENWIIF3
    masterConfig.serialConfig.portConfigs[2].functionMask = FUNCTION_RX_SERIAL;
    masterConfig.batteryConfig.vbatscale = 20;
#else
    masterConfig.serialConfig.portConfigs[1].functionMask = FUNCTION_RX_SERIAL;
#endif
    masterConfig.rxConfig.serialrx_provider = 1;
    masterConfig.rxConfig.spektrum_sat_bind = 5;
    masterConfig.escAndServoConfig.minthrottle = 1000;
    masterConfig.escAndServoConfig.maxthrottle = 2000;
    masterConfig.motor_pwm_rate = 32000;
    masterConfig.looptime = 2000;
    currentProfile->pidProfile.P8[ROLL] = 36;
    currentProfile->pidProfile.P8[PITCH] = 36;
    masterConfig.failsafeConfig.failsafe_delay = 2;
    masterConfig.failsafeConfig.failsafe_off_delay = 0;
    currentControlRateProfile->rcRate8 = 130;
    currentControlRateProfile->rates[FD_PITCH] = 20;
    currentControlRateProfile->rates[FD_ROLL] = 20;
    currentControlRateProfile->rates[FD_YAW] = 100;
    parseRcChannels("TAER1234", &masterConfig.rxConfig);

    //  { 1.0f, -0.414178f,  1.0f, -1.0f },          // REAR_R
    masterConfig.customMotorMixer[0].throttle = 1.0f;
    masterConfig.customMotorMixer[0].roll = -0.414178f;
    masterConfig.customMotorMixer[0].pitch = 1.0f;
    masterConfig.customMotorMixer[0].yaw = -1.0f;

    //  { 1.0f, -0.414178f, -1.0f,  1.0f },          // FRONT_R
    masterConfig.customMotorMixer[1].throttle = 1.0f;
    masterConfig.customMotorMixer[1].roll = -0.414178f;
    masterConfig.customMotorMixer[1].pitch = -1.0f;
    masterConfig.customMotorMixer[1].yaw = 1.0f;

    //  { 1.0f,  0.414178f,  1.0f,  1.0f },          // REAR_L
    masterConfig.customMotorMixer[2].throttle = 1.0f;
    masterConfig.customMotorMixer[2].roll = 0.414178f;
    masterConfig.customMotorMixer[2].pitch = 1.0f;
    masterConfig.customMotorMixer[2].yaw = 1.0f;

    //  { 1.0f,  0.414178f, -1.0f, -1.0f },          // FRONT_L
    masterConfig.customMotorMixer[3].throttle = 1.0f;
    masterConfig.customMotorMixer[3].roll = 0.414178f;
    masterConfig.customMotorMixer[3].pitch = -1.0f;
    masterConfig.customMotorMixer[3].yaw = -1.0f;

    //  { 1.0f, -1.0f, -0.414178f, -1.0f },          // MIDFRONT_R
    masterConfig.customMotorMixer[4].throttle = 1.0f;
    masterConfig.customMotorMixer[4].roll = -1.0f;
    masterConfig.customMotorMixer[4].pitch = -0.414178f;
    masterConfig.customMotorMixer[4].yaw = -1.0f;

    //  { 1.0f,  1.0f, -0.414178f,  1.0f },          // MIDFRONT_L
    masterConfig.customMotorMixer[5].throttle = 1.0f;
    masterConfig.customMotorMixer[5].roll = 1.0f;
    masterConfig.customMotorMixer[5].pitch = -0.414178f;
    masterConfig.customMotorMixer[5].yaw = 1.0f;

    //  { 1.0f, -1.0f,  0.414178f,  1.0f },          // MIDREAR_R
    masterConfig.customMotorMixer[6].throttle = 1.0f;
    masterConfig.customMotorMixer[6].roll = -1.0f;
    masterConfig.customMotorMixer[6].pitch = 0.414178f;
    masterConfig.customMotorMixer[6].yaw = 1.0f;

    //  { 1.0f,  1.0f,  0.414178f, -1.0f },          // MIDREAR_L
    masterConfig.customMotorMixer[7].throttle = 1.0f;
    masterConfig.customMotorMixer[7].roll = 1.0f;
    masterConfig.customMotorMixer[7].pitch = 0.414178f;
    masterConfig.customMotorMixer[7].yaw = -1.0f;
#endif

    // copy first profile into remaining profile
    for (i = 1; i < MAX_PROFILE_COUNT; i++) {
        memcpy(&masterConfig.profile[i], currentProfile, sizeof(profile_t));
    }

    // copy first control rate config into remaining profile
    for (i = 1; i < MAX_CONTROL_RATE_PROFILE_COUNT; i++) {
        memcpy(&masterConfig.controlRateProfiles[i], currentControlRateProfile, sizeof(controlRateConfig_t));
    }

    for (i = 1; i < MAX_PROFILE_COUNT; i++) {
        masterConfig.profile[i].defaultRateProfileIndex = i % MAX_CONTROL_RATE_PROFILE_COUNT;
    }
}
예제 #8
0
// Default settings
static void resetConf(void)
{
    int i;
    const int8_t default_align[3][3] = { /* GYRO */ { 0, 0, 0 }, /* ACC */ { 0, 0, 0 }, /* MAG */ { -2, -3, 1 } };

    memset(&cfg, 0, sizeof(config_t));

    cfg.version = EEPROM_CONF_VERSION;
    //cfg.mixerConfiguration = MULTITYPE_QUADX;
    cfg.mixerConfiguration = MULTITYPE_AIRPLANE;
    featureClearAll();
    //featureSet(FEATURE_VBAT);		// Enable Vbat monitoring
    //featureSet(FEATURE_PPM);	  	// Enable CPPM input

    cfg.looptime = 0;
    cfg.P8[ROLL] = 20;
    //cfg.I8[ROLL] = 30;
    //cfg.D8[ROLL] = 23;
    cfg.I8[ROLL] = 0;
    cfg.D8[ROLL] = 0;
    cfg.P8[PITCH] = 20;
    //cfg.I8[PITCH] = 30;
    //cfg.D8[PITCH] = 23;
    cfg.I8[PITCH] = 0;
    cfg.D8[PITCH] = 0;
    cfg.P8[YAW] = 85;
    cfg.I8[YAW] = 0;
    //cfg.I8[YAW] = 45;
    cfg.D8[YAW] = 0;
    cfg.P8[PIDALT] = 0;
    cfg.I8[PIDALT] = 0;
    cfg.D8[PIDALT] = 0;
    cfg.P8[PIDPOS] = 0; 	// POSHOLD_P * 100;
    cfg.I8[PIDPOS] = 0; 	// POSHOLD_I * 100;
    cfg.D8[PIDPOS] = 0;
    cfg.P8[PIDPOSR] = 0; 	// POSHOLD_RATE_P * 10;
    cfg.I8[PIDPOSR] = 0; 	// POSHOLD_RATE_I * 100;
    cfg.D8[PIDPOSR] = 0; 	// POSHOLD_RATE_D * 1000;
    cfg.P8[PIDNAVR] = 0; 	// NAV_P * 10;
    cfg.I8[PIDNAVR] = 0; 	// NAV_I * 100;
    cfg.D8[PIDNAVR] = 0; 	// NAV_D * 1000;
    cfg.P8[PIDLEVEL] = 20;
    cfg.I8[PIDLEVEL] = 0;
    cfg.D8[PIDLEVEL] = 100;
    //cfg.P8[PIDLEVEL] = 70;
    //cfg.I8[PIDLEVEL] = 10;
    //cfg.D8[PIDLEVEL] = 20;
    cfg.P8[PIDMAG] = 40;
    cfg.P8[PIDVEL] = 0;
    cfg.I8[PIDVEL] = 0;
    cfg.D8[PIDVEL] = 0;
    cfg.rcRate8 = 100;
    cfg.rcExpo8 = 0;
    cfg.rollPitchRate = 0;
    cfg.yawRate = 0;
    cfg.dynThrPID = 0;
    cfg.thrMid8 = 50;
    cfg.thrExpo8 = 0;
    for (i = 0; i < CHECKBOXITEMS; i++)
        cfg.activate[i] = 0;
    cfg.angleTrim[0] = 0;
    cfg.angleTrim[1] = 0;
    cfg.accZero[0] = 0;
    cfg.accZero[1] = 0;
    cfg.accZero[2] = 0;
    // Magnetic declination: format is [sign]dddmm (degreesminutes) default is zero.
    // +12deg 31min = 1231 Sydney, Australia
    // -6deg 37min = -637 Southern Japan
    // cfg.mag_declination = 0;
    cfg.mag_declination = 1231;
    memcpy(&cfg.align, default_align, sizeof(cfg.align));
    cfg.acc_hardware = ACC_DEFAULT;     // default/autodetect
    cfg.acc_lpf_factor = 4;
    cfg.acc_lpf_for_velocity = 10;
    cfg.accz_deadband = 50;
    cfg.gyro_cmpf_factor = 400; 		// default MWC
    cfg.gyro_lpf = 42;
    cfg.mpu6050_scale = 1; // f**k invensense
    cfg.baro_tab_size = 21;
    cfg.baro_noise_lpf = 0.6f;
    cfg.baro_cf = 0.985f;
    cfg.moron_threshold = 32;
    cfg.gyro_smoothing_factor = 0x00141403;     // default factors of 20, 20, 3 for R/P/Y
    cfg.vbatscale = 110;
    cfg.vbatmaxcellvoltage = 43;
    cfg.vbatmincellvoltage = 33;
    // cfg.power_adc_channel = 0;

    // Radio
    parseRcChannels("AETR1234");
    //parseRcChannels("TAER1234"); // Debug - JR
    cfg.deadband = 0;
    cfg.yawdeadband = 0;
    cfg.alt_hold_throttle_neutral = 20;
    cfg.spektrum_hires = 0;
    for (i = 0; i < 8; i++)					// RC stick centers
    {
        cfg.midrc[i] = 1500;
    }
    cfg.defaultrc = 1500;
    cfg.mincheck = 1100;
    cfg.maxcheck = 1900;
    cfg.retarded_arm = 0;       			// disable arm/disarm on roll left/right

    // Failsafe Variables
    cfg.failsafe_delay = 10;    			// 1sec
    cfg.failsafe_off_delay = 200;       	// 20sec
    cfg.failsafe_throttle = 1200;       	// decent default which should always be below hover throttle for people.

    // Motor/ESC/Servo
    cfg.minthrottle = 1150;
    cfg.maxthrottle = 1850;
    cfg.mincommand = 1000;
    cfg.motor_pwm_rate = 400;
    cfg.servo_pwm_rate = 50;

    // servos
    cfg.yaw_direction = 1;
    cfg.tri_yaw_middle = 1500;
    cfg.tri_yaw_min = 1020;
    cfg.tri_yaw_max = 2000;

    // gimbal
    cfg.gimbal_pitch_gain = 10;
    cfg.gimbal_roll_gain = 10;
    cfg.gimbal_flags = GIMBAL_NORMAL;
    cfg.gimbal_pitch_min = 1020;
    cfg.gimbal_pitch_max = 2000;
    cfg.gimbal_pitch_mid = 1500;
    cfg.gimbal_roll_min = 1020;
    cfg.gimbal_roll_max = 2000;
    cfg.gimbal_roll_mid = 1500;

    // gps/nav stuff
    cfg.gps_type = GPS_NMEA;
    cfg.gps_baudrate = 115200;
    cfg.gps_wp_radius = 200;
    cfg.gps_lpf = 20;
    cfg.nav_slew_rate = 30;
    cfg.nav_controls_heading = 1;
    cfg.nav_speed_min = 100;
    cfg.nav_speed_max = 300;

    // serial (USART1) baudrate
    cfg.serial_baudrate = 115200;

    // Aeroplane stuff
    cfg.flapmode = ADV_FLAP;				// Switch for flaperon mode?
    cfg.flapchan = AUX2;					// RC channel number for simple flaps)
    cfg.aileron2 = AUX1;					// RC channel number for second aileron
    cfg.flapspeed = 10;						// Desired rate of change of flaps
    cfg.flapstep = 3;						// Steps for each flap movement
    cfg.DynPIDchan = THROTTLE;				// Dynamic PID source channel
    cfg.DynPIDbreakpoint = 1500;			// Dynamic PID breakpoint
    cfg.rollPIDpol = 1;
    cfg.pitchPIDpol = 1;
    cfg.yawPIDpol = 1;

    for (i = 0; i < 8; i++)					// Servo limits
    {
        cfg.servoendpoint_low[i] = 1000;
        cfg.servoendpoint_high[i] = 2000;
        cfg.servoreverse[i] = 1;
        cfg.servotrim[i] = 1500;			// Set servo trim to default
    }

    // custom mixer. clear by defaults.
    for (i = 0; i < MAX_MOTORS; i++)
        cfg.customMixer[i].throttle = 0.0f;

    writeParams(0);
}
예제 #9
0
// Default settings
static void resetConf(void)
{
    int i;
#ifdef USE_SERVOS
    int8_t servoRates[MAX_SUPPORTED_SERVOS] = { 30, 30, 100, 100, 100, 100, 100, 100 };
    ;
#endif

    // Clear all configuration
    memset(&masterConfig, 0, sizeof(master_t));
    setProfile(0);
    setControlRateProfile(0);

    masterConfig.version = EEPROM_CONF_VERSION;
    masterConfig.mixerMode = MIXER_QUADX;
    featureClearAll();
#if defined(CJMCU) || defined(SPARKY)
    featureSet(FEATURE_RX_PPM);
#endif

#ifdef BOARD_HAS_VOLTAGE_DIVIDER
    // only enable the VBAT feature by default if the board has a voltage divider otherwise
    // the user may see incorrect readings and unexpected issues with pin mappings may occur.
    featureSet(FEATURE_VBAT);
#endif

    featureSet(FEATURE_FAILSAFE);

    // global settings
    masterConfig.current_profile_index = 0;     // default profile
    masterConfig.gyro_cmpf_factor = 600;        // default MWC
    masterConfig.gyro_cmpfm_factor = 250;       // default MWC
    masterConfig.gyro_lpf = 42;                 // supported by all gyro drivers now. In case of ST gyro, will default to 32Hz instead

    resetAccelerometerTrims(&masterConfig.accZero);

    resetSensorAlignment(&masterConfig.sensorAlignmentConfig);

    masterConfig.boardAlignment.rollDegrees = 0;
    masterConfig.boardAlignment.pitchDegrees = 0;
    masterConfig.boardAlignment.yawDegrees = 0;
    masterConfig.acc_hardware = ACC_DEFAULT;     // default/autodetect
    masterConfig.max_angle_inclination = 500;    // 50 degrees
    masterConfig.yaw_control_direction = 1;
    masterConfig.gyroConfig.gyroMovementCalibrationThreshold = 32;

    masterConfig.mag_hardware = MAG_DEFAULT;     // default/autodetect

    resetBatteryConfig(&masterConfig.batteryConfig);

    resetTelemetryConfig(&masterConfig.telemetryConfig);

    masterConfig.rxConfig.serialrx_provider = 0;
    masterConfig.rxConfig.spektrum_sat_bind = 0;
    masterConfig.rxConfig.midrc = 1500;
    masterConfig.rxConfig.mincheck = 1100;
    masterConfig.rxConfig.maxcheck = 1900;
    masterConfig.rxConfig.rx_min_usec = 985;          // any of first 4 channels below this value will trigger rx loss detection
    masterConfig.rxConfig.rx_max_usec = 2115;         // any of first 4 channels above this value will trigger rx loss detection

    masterConfig.rxConfig.rssi_channel = 0;
    masterConfig.rxConfig.rssi_scale = RSSI_SCALE_DEFAULT;

    masterConfig.inputFilteringMode = INPUT_FILTERING_DISABLED;

    masterConfig.retarded_arm = 0;
    masterConfig.disarm_kill_switch = 1;
    masterConfig.auto_disarm_delay = 5;
    masterConfig.small_angle = 25;

    resetMixerConfig(&masterConfig.mixerConfig);

    masterConfig.airplaneConfig.flaps_speed = 0;
    masterConfig.airplaneConfig.fixedwing_althold_dir = 1;

    // Motor/ESC/Servo
    resetEscAndServoConfig(&masterConfig.escAndServoConfig);
    resetFlight3DConfig(&masterConfig.flight3DConfig);

#ifdef BRUSHED_MOTORS
    masterConfig.motor_pwm_rate = BRUSHED_MOTORS_PWM_RATE;
#else
    masterConfig.motor_pwm_rate = BRUSHLESS_MOTORS_PWM_RATE;
#endif
    masterConfig.servo_pwm_rate = 50;

#ifdef GPS
    // gps/nav stuff
    masterConfig.gpsConfig.provider = GPS_NMEA;
    masterConfig.gpsConfig.sbasMode = SBAS_AUTO;
    masterConfig.gpsConfig.autoConfig = GPS_AUTOCONFIG_ON;
    masterConfig.gpsConfig.autoBaud = GPS_AUTOBAUD_OFF;
#endif

    resetSerialConfig(&masterConfig.serialConfig);

    masterConfig.looptime = 3500;
    masterConfig.emf_avoidance = 0;

    resetPidProfile(&currentProfile->pidProfile);

    resetControlRateConfig(&masterConfig.controlRateProfiles[0]);

    // for (i = 0; i < CHECKBOXITEMS; i++)
    //     cfg.activate[i] = 0;

    resetRollAndPitchTrims(&currentProfile->accelerometerTrims);

    currentProfile->mag_declination = 0;
    currentProfile->acc_lpf_factor = 4;
    currentProfile->accz_lpf_cutoff = 5.0f;
    currentProfile->accDeadband.xy = 40;
    currentProfile->accDeadband.z = 40;

    resetBarometerConfig(&currentProfile->barometerConfig);

    currentProfile->acc_unarmedcal = 1;

    // Radio
    parseRcChannels("AETR1234", &masterConfig.rxConfig);

    resetRcControlsConfig(&currentProfile->rcControlsConfig);

    currentProfile->throttle_correction_value = 0;      // could 10 with althold or 40 for fpv
    currentProfile->throttle_correction_angle = 800;    // could be 80.0 deg with atlhold or 45.0 for fpv

    // Failsafe Variables
    masterConfig.failsafeConfig.failsafe_delay = 10;              // 1sec
    masterConfig.failsafeConfig.failsafe_off_delay = 200;         // 20sec
    masterConfig.failsafeConfig.failsafe_throttle = 1000;         // default throttle off.

#ifdef USE_SERVOS
    // servos
    for (i = 0; i < MAX_SUPPORTED_SERVOS; i++) {
        currentProfile->servoConf[i].min = DEFAULT_SERVO_MIN;
        currentProfile->servoConf[i].max = DEFAULT_SERVO_MAX;
        currentProfile->servoConf[i].middle = DEFAULT_SERVO_MIDDLE;
        currentProfile->servoConf[i].rate = servoRates[i];
        currentProfile->servoConf[i].forwardFromChannel = CHANNEL_FORWARDING_DISABLED;
    }

    // gimbal
    currentProfile->gimbalConfig.gimbal_flags = GIMBAL_NORMAL;
#endif

#ifdef GPS
    resetGpsProfile(&currentProfile->gpsProfile);
#endif

    // custom mixer. clear by defaults.
    for (i = 0; i < MAX_SUPPORTED_MOTORS; i++)
        masterConfig.customMixer[i].throttle = 0.0f;

#ifdef LED_STRIP
    applyDefaultColors(masterConfig.colors, CONFIGURABLE_COLOR_COUNT);
    applyDefaultLedStripConfig(masterConfig.ledConfigs);
#endif

#ifdef BLACKBOX
#ifdef SPRACINGF3
    featureSet(FEATURE_BLACKBOX);
    masterConfig.blackbox_device = 1;
#else
    masterConfig.blackbox_device = 0;
#endif
    masterConfig.blackbox_rate_num = 1;
    masterConfig.blackbox_rate_denom = 1;
#endif

    // alternative defaults settings for ALIENWIIF1 and ALIENWIIF3 targets
#ifdef ALIENWII32
    featureSet(FEATURE_RX_SERIAL);
    featureSet(FEATURE_MOTOR_STOP);
    featureSet(FEATURE_FAILSAFE);
#ifdef ALIENWIIF3
    masterConfig.serialConfig.portConfigs[2].functionMask = FUNCTION_RX_SERIAL;
    masterConfig.batteryConfig.vbatscale = 20;
#else
    masterConfig.serialConfig.portConfigs[1].functionMask = FUNCTION_RX_SERIAL;
#endif
    masterConfig.rxConfig.serialrx_provider = 1;
    masterConfig.rxConfig.spektrum_sat_bind = 5;
    masterConfig.escAndServoConfig.minthrottle = 1000;
    masterConfig.escAndServoConfig.maxthrottle = 2000;
    masterConfig.motor_pwm_rate = 32000;
    masterConfig.looptime = 2000;
    currentProfile->pidProfile.pidController = 3;
    currentProfile->pidProfile.P8[ROLL] = 36;
    currentProfile->pidProfile.P8[PITCH] = 36;
    masterConfig.failsafeConfig.failsafe_delay = 2;
    masterConfig.failsafeConfig.failsafe_off_delay = 0;
    masterConfig.failsafeConfig.failsafe_throttle = 1000;
    currentControlRateProfile->rcRate8 = 130;
    currentControlRateProfile->rates[FD_PITCH] = 20;
    currentControlRateProfile->rates[FD_ROLL] = 20;
    currentControlRateProfile->rates[FD_YAW] = 100;
    parseRcChannels("TAER1234", &masterConfig.rxConfig);

    //  { 1.0f, -0.5f,  1.0f, -1.0f },          // REAR_R
    masterConfig.customMixer[0].throttle = 1.0f;
    masterConfig.customMixer[0].roll = -0.5f;
    masterConfig.customMixer[0].pitch = 1.0f;
    masterConfig.customMixer[0].yaw = -1.0f;

    //  { 1.0f, -0.5f, -1.0f,  1.0f },          // FRONT_R
    masterConfig.customMixer[1].throttle = 1.0f;
    masterConfig.customMixer[1].roll = -0.5f;
    masterConfig.customMixer[1].pitch = -1.0f;
    masterConfig.customMixer[1].yaw = 1.0f;

    //  { 1.0f,  0.5f,  1.0f,  1.0f },          // REAR_L
    masterConfig.customMixer[2].throttle = 1.0f;
    masterConfig.customMixer[2].roll = 0.5f;
    masterConfig.customMixer[2].pitch = 1.0f;
    masterConfig.customMixer[2].yaw = 1.0f;

    //  { 1.0f,  0.5f, -1.0f, -1.0f },          // FRONT_L
    masterConfig.customMixer[3].throttle = 1.0f;
    masterConfig.customMixer[3].roll = 0.5f;
    masterConfig.customMixer[3].pitch = -1.0f;
    masterConfig.customMixer[3].yaw = -1.0f;

    //  { 1.0f, -1.0f, -0.5f, -1.0f },          // MIDFRONT_R
    masterConfig.customMixer[4].throttle = 1.0f;
    masterConfig.customMixer[4].roll = -1.0f;
    masterConfig.customMixer[4].pitch = -0.5f;
    masterConfig.customMixer[4].yaw = -1.0f;

    //  { 1.0f,  1.0f, -0.5f,  1.0f },          // MIDFRONT_L
    masterConfig.customMixer[5].throttle = 1.0f;
    masterConfig.customMixer[5].roll = 1.0f;
    masterConfig.customMixer[5].pitch = -0.5f;
    masterConfig.customMixer[5].yaw = 1.0f;

    //  { 1.0f, -1.0f,  0.5f,  1.0f },          // MIDREAR_R
    masterConfig.customMixer[6].throttle = 1.0f;
    masterConfig.customMixer[6].roll = -1.0f;
    masterConfig.customMixer[6].pitch = 0.5f;
    masterConfig.customMixer[6].yaw = 1.0f;

    //  { 1.0f,  1.0f,  0.5f, -1.0f },          // MIDREAR_L
    masterConfig.customMixer[7].throttle = 1.0f;
    masterConfig.customMixer[7].roll = 1.0f;
    masterConfig.customMixer[7].pitch = 0.5f;
    masterConfig.customMixer[7].yaw = -1.0f;
#endif

    // copy first profile into remaining profile
    for (i = 1; i < MAX_PROFILE_COUNT; i++) {
        memcpy(&masterConfig.profile[i], currentProfile, sizeof(profile_t));
    }

    // copy first control rate config into remaining profile
    for (i = 1; i < MAX_CONTROL_RATE_PROFILE_COUNT; i++) {
        memcpy(&masterConfig.controlRateProfiles[i], currentControlRateProfile, sizeof(controlRateConfig_t));
    }

    for (i = 1; i < MAX_PROFILE_COUNT; i++) {
        masterConfig.profile[i].defaultRateProfileIndex = i % MAX_CONTROL_RATE_PROFILE_COUNT;
    }
}
예제 #10
0
// Default settings
STATIC_UNIT_TESTED void resetConf(void)
{
    pgResetAll(MAX_PROFILE_COUNT);

    setProfile(0);
    pgActivateProfile(0);

    setControlRateProfile(0);

    parseRcChannels("AETR1234", rxConfig());

    featureClearAll();

    featureSet(DEFAULT_RX_FEATURE | FEATURE_FAILSAFE | FEATURE_BLACKBOX);
#ifdef DEFAULT_FEATURES
    featureSet(DEFAULT_FEATURES);
#endif

#ifdef BOARD_HAS_VOLTAGE_DIVIDER
    // only enable the feature by default if the board has supporting hardware
    featureSet(FEATURE_VBAT);
#endif

#ifdef BOARD_HAS_AMPERAGE_METER
    // only enable the feature by default if the board has supporting hardware
    featureSet(FEATURE_AMPERAGE_METER);
    batteryConfig()->amperageMeterSource = AMPERAGE_METER_ADC;
#endif

    // alternative defaults settings for ALIENFLIGHTF1 and ALIENFLIGHTF3 targets
#ifdef ALIENFLIGHT
#ifdef ALIENFLIGHTF3
    serialConfig()->portConfigs[2].functionMask = FUNCTION_RX_SERIAL;
    getVoltageMeterConfig(ADC_BATTERY)->vbatscale = 20;
    sensorSelectionConfig()->mag_hardware = MAG_NONE;            // disabled by default
# else
    serialConfig()->portConfigs[1].functionMask = FUNCTION_RX_SERIAL;
# endif
    rxConfig()->serialrx_provider = SERIALRX_SPEKTRUM2048;
    rxConfig()->spektrum_sat_bind = 5;
    motorConfig()->minthrottle = 1000;
    motorConfig()->maxthrottle = 2000;
    motorConfig()->motor_pwm_rate = 32000;
    failsafeConfig()->failsafe_delay = 2;
    failsafeConfig()->failsafe_off_delay = 0;
    mixerConfig()->yaw_jump_prevention_limit = YAW_JUMP_PREVENTION_LIMIT_HIGH;
    currentControlRateProfile->rcRate8 = 100;
    currentControlRateProfile->rates[PITCH] = 20;
    currentControlRateProfile->rates[ROLL] = 20;
    currentControlRateProfile->rates[YAW] = 20;
    parseRcChannels("TAER1234", rxConfig());

    *customMotorMixer(0) = (motorMixer_t){ 1.0f, -0.414178f,  1.0f, -1.0f };    // REAR_R
    *customMotorMixer(1) = (motorMixer_t){ 1.0f, -0.414178f, -1.0f,  1.0f };    // FRONT_R
    *customMotorMixer(2) = (motorMixer_t){ 1.0f,  0.414178f,  1.0f,  1.0f };    // REAR_L
    *customMotorMixer(3) = (motorMixer_t){ 1.0f,  0.414178f, -1.0f, -1.0f };    // FRONT_L
    *customMotorMixer(4) = (motorMixer_t){ 1.0f, -1.0f, -0.414178f, -1.0f };    // MIDFRONT_R
    *customMotorMixer(5) = (motorMixer_t){ 1.0f,  1.0f, -0.414178f,  1.0f };    // MIDFRONT_L
    *customMotorMixer(6) = (motorMixer_t){ 1.0f, -1.0f,  0.414178f,  1.0f };    // MIDREAR_R
    *customMotorMixer(7) = (motorMixer_t){ 1.0f,  1.0f,  0.414178f, -1.0f };    // MIDREAR_L
#endif

    // copy first profile into remaining profile
    PG_FOREACH_PROFILE(reg) {
        for (int i = 1; i < MAX_PROFILE_COUNT; i++) {
            memcpy(reg->address + i * pgSize(reg), reg->address, pgSize(reg));
        }
    }
    for (int i = 1; i < MAX_PROFILE_COUNT; i++) {
        configureRateProfileSelection(i, i % MAX_CONTROL_RATE_PROFILE_COUNT);
    }
}
예제 #11
0
// Default settings
static void resetConf(void)
{
    int32_t i;
    memset(&cfg, 0, sizeof(config_t));
    
    cfg.version = EEPROM_CONF_VERSION;

	// Default settings
    cfg.version = EEPROM_CONF_VERSION;
    cfg.mixerConfiguration                 = MULTITYPE_QUADX;
    
    featureClearAll();
    featureSet(FEATURE_VBAT);
    featureSet(FEATURE_PPM);
    
    parseRcChannels("AETR1234");
    
    // Motor/ESC
    cfg.escPwmRate                     = 400;
    cfg.servoPwmRate                   = 50;
    
    // Failsafe
    cfg.failsafeOnDelay                = 50; // Number of command loops (50Hz) until failsafe kicks in
    cfg.failsafeOffDelay               = 20000; // Number of command loops until failsafe stops
    cfg.failsafeThrottle               = 1200;
    
    cfg.commandRate             = 90;
    cfg.commandExpo             = 65;
    cfg.rollPitchRate           = 0;
    cfg.yawRate                 = 0;
    //cfg.dynThrPID             = 0;
    cfg.throttleMid             = 50;
    cfg.throttleExpo            = 0;
    
    // Command Settings
    for(i = 0; i < AUX_OPTIONS; ++i)
        cfg.auxActivate[i] = 0;

    cfg.minCommand                         = 1000;
    cfg.midCommand                         = 1500;
    cfg.maxCommand                         = 2000;
    cfg.minCheck                           = 1100;
    cfg.maxCheck                           = 1900;
    cfg.minThrottle                        = 1150;
    cfg.maxThrottle                        = 1850;
    cfg.spektrumHiRes                      = false;
    
    cfg.deadBand[ROLL]                     = 12;
    cfg.deadBand[PITCH]                    = 12;
    cfg.deadBand[YAW]                      = 12;
    
    // Servos
    
    // Tricopter
    cfg.yawDirection                       = 1;
    cfg.triYawServoMin                     = 1000;
    cfg.triYawServoMid                     = 1500;
    cfg.triYawServoMax                     = 2000;
    
    // Bicopter
    cfg.biLeftServoMin                     = 1000;
    cfg.biLeftServoMid                     = 1500;
    cfg.biLeftServoMax                     = 2000;

    cfg.biRightServoMin                    = 1000;
    cfg.biRightServoMid                    = 1500;
    cfg.biRightServoMax                    = 2000;
    
    // Flying wing
    cfg.wingLeftMin             = 1020;
    cfg.wingLeftMid             = 1500;
    cfg.wingLeftMax             = 2000;
    cfg.wingRightMin            = 1020;
    cfg.wingRightMid            = 1500;
    cfg.wingRightMax            = 2000;
    cfg.pitchDirectionLeft      = 1;
    cfg.pitchDirectionRight     = -1;
    cfg.rollDirectionLeft       = 1;
    cfg.rollDirectionRight      = 1;
    
    cfg.gimbalFlags = GIMBAL_NORMAL;
    cfg.gimbalSmoothFactor = 0.95f;

    cfg.gimbalRollServoMin                 = 1000;
	cfg.gimbalRollServoMid                 = 1500;
	cfg.gimbalRollServoMax                 = 2000;
	cfg.gimbalRollServoGain                = 1.0f;

	cfg.gimbalPitchServoMin                = 1000;
	cfg.gimbalPitchServoMid                = 1500;
	cfg.gimbalPitchServoMax                = 2000;
	cfg.gimbalPitchServoGain               = 1.0f;

    // PIDs
    cfg.pids[ROLL_RATE_PID].p               = 100.0f;
    cfg.pids[ROLL_RATE_PID].i               =   0.0f;
    cfg.pids[ROLL_RATE_PID].d               =   0.0f;
    cfg.pids[ROLL_RATE_PID].iLim            = 100.0f;  // PWMs

    cfg.pids[PITCH_RATE_PID].p              = 100.0f;
    cfg.pids[PITCH_RATE_PID].i              =   0.0f;
    cfg.pids[PITCH_RATE_PID].d              =   0.0f;
    cfg.pids[PITCH_RATE_PID].iLim           = 100.0f;  // PWMs

    cfg.pids[YAW_RATE_PID].p                = 200.0f;
    cfg.pids[YAW_RATE_PID].i                =   0.0f;
    cfg.pids[YAW_RATE_PID].d                =   0.0f;
    cfg.pids[YAW_RATE_PID].iLim             = 100.0f;  // PWMs

    cfg.pids[ROLL_LEVEL_PID].p                =   2.0f;
    cfg.pids[ROLL_LEVEL_PID].i                =   0.0f;
    cfg.pids[ROLL_LEVEL_PID].d                =   0.0f;
    cfg.pids[ROLL_LEVEL_PID].iLim             =   0.5f;  // radians/sec

    cfg.pids[PITCH_LEVEL_PID].p               =   2.0f;
    cfg.pids[PITCH_LEVEL_PID].i               =   0.0f;
    cfg.pids[PITCH_LEVEL_PID].d               =   0.0f;
    cfg.pids[PITCH_LEVEL_PID].iLim            =   0.5f;  // radians/sec

    cfg.pids[HEADING_PID].p                 =   1.5f;
    cfg.pids[HEADING_PID].i                 =   0.0f;
    cfg.pids[HEADING_PID].d                 =   0.0f;
    cfg.pids[HEADING_PID].iLim              =   0.5f;  // radians/sec
    
    cfg.pids[ALTITUDE_PID].p                 =   20.0f;
    cfg.pids[ALTITUDE_PID].i                 =   17.0f;
    cfg.pids[ALTITUDE_PID].d                 =   7.0f;
    cfg.pids[ALTITUDE_PID].iLim              =   30000.0f; // 0.1 m
    
    cfg.angleTrim[ROLL]         = 0.0f;
    cfg.angleTrim[PITCH]        = 0.0f;
    
    cfg.accelLPF                = false;
    cfg.accelSmoothFactor       = 0.75f;
    
    cfg.accelCalibrated                 = false;
    cfg.accelBias[XAXIS]                = 0;
    cfg.accelBias[YAXIS]                = 0;
    cfg.accelBias[ZAXIS]                = 0;

    cfg.gyroBiasOnStartup           = false;
    cfg.gyroSmoothFactor            = 0.95f;
    cfg.gyroTCBiasSlope[ROLL]       = 0.0f;
    cfg.gyroTCBiasSlope[PITCH]      = 0.0f;
    cfg.gyroTCBiasSlope[YAW]        = 0.0f;
    cfg.gyroTCBiasIntercept[ROLL]   = 0.0f;
    cfg.gyroTCBiasIntercept[PITCH]  = 0.0f;
    cfg.gyroTCBiasIntercept[YAW]    = 0.0f;

    cfg.magCalibrated               = false;
    cfg.magBias[ROLL]               = 0;
    cfg.magBias[PITCH]              = 0;
    cfg.magBias[YAW]                = 0;
    
    cfg.mpu6050Scale                = false; // Shitty hack

    // For Mahony AHRS
    
    cfg.accelKp                     = 2.0f;
    cfg.accelKi                     = 0.01f;
    
    cfg.magKp                       = 1.0f;
    cfg.magKi                       = 0.01f;
    
    cfg.magDriftCompensation        = false;

    // Get your magnetic decliniation from here : http://magnetic-declination.com/
    // For example, -6deg 37min, = -6.37 Japan, format is [sign]ddd.mm (degreesminutes)
    cfg.magDeclination              = 10.59f; 

    cfg.batScale                    = 11.0f;
    cfg.batMinCellVoltage           = 3.3f;
    cfg.batMaxCellVoltage           = 4.2f;
    
    cfg.startupDelay                = 1000;
    
    // custom mixer. clear by defaults.
    for (i = 0; i < MAX_MOTORS; i++)
        cfg.customMixer[i].throttle = 0.0f;

    writeParams();
}
예제 #12
0
파일: config.c 프로젝트: jeyong/cleanflight
// Default settings
STATIC_UNIT_TESTED void resetConf(void)
{
    pgResetAll(MAX_PROFILE_COUNT);

    setProfile(0);
    pgActivateProfile(0);

    setControlRateProfile(0);

    featureClearAll();

    featureSet(DEFAULT_RX_FEATURE);

#ifdef BOARD_HAS_VOLTAGE_DIVIDER
    // only enable the VBAT feature by default if the board has a voltage divider otherwise
    // the user may see incorrect readings and unexpected issues with pin mappings may occur.
    featureSet(FEATURE_VBAT);
#endif

    featureSet(FEATURE_FAILSAFE);

    parseRcChannels("AETR1234", rxConfig());

    featureSet(FEATURE_BLACKBOX);

#if defined(COLIBRI_RACE)
    // alternative defaults settings for COLIBRI RACE targets
    imuConfig()->looptime = 1000;
    featureSet(FEATURE_ONESHOT125);
    featureSet(FEATURE_LED_STRIP);
#endif

#ifdef SPRACINGF3EVO
    featureSet(FEATURE_TRANSPONDER);
    featureSet(FEATURE_RSSI_ADC);
    featureSet(FEATURE_CURRENT_METER);
    featureSet(FEATURE_TELEMETRY);
#endif

    // alternative defaults settings for ALIENWIIF1 and ALIENWIIF3 targets
#ifdef ALIENWII32
    featureSet(FEATURE_RX_SERIAL);
    featureSet(FEATURE_MOTOR_STOP);
# ifdef ALIENWIIF3
    serialConfig()->portConfigs[2].functionMask = FUNCTION_RX_SERIAL;
    batteryConfig()->vbatscale = 20;
# else
    serialConfig()->portConfigs[1].functionMask = FUNCTION_RX_SERIAL;
# endif
    rxConfig()->serialrx_provider = SERIALRX_SPEKTRUM2048;
    rxConfig()->spektrum_sat_bind = 5;
    motorAndServoConfig()->minthrottle = 1000;
    motorAndServoConfig()->maxthrottle = 2000;
    motorAndServoConfig()->motor_pwm_rate = 32000;
    imuConfig()->looptime = 2000;
    pidProfile()->pidController = 3;
    pidProfile()->P8[PIDROLL] = 36;
    pidProfile()->P8[PIDPITCH] = 36;
    failsafeConfig()->failsafe_delay = 2;
    failsafeConfig()->failsafe_off_delay = 0;
    currentControlRateProfile->rcRate8 = 130;
    currentControlRateProfile->rates[ROLL] = 20;
    currentControlRateProfile->rates[PITCH] = 20;
    currentControlRateProfile->rates[YAW] = 100;
    parseRcChannels("TAER1234", rxConfig());
    *customMotorMixer(0) = (motorMixer_t){ 1.0f, -0.414178f,  1.0f, -1.0f };    // REAR_R
    *customMotorMixer(1) = (motorMixer_t){ 1.0f, -0.414178f, -1.0f,  1.0f };    // FRONT_R
    *customMotorMixer(2) = (motorMixer_t){ 1.0f,  0.414178f,  1.0f,  1.0f };    // REAR_L
    *customMotorMixer(3) = (motorMixer_t){ 1.0f,  0.414178f, -1.0f, -1.0f };    // FRONT_L
    *customMotorMixer(4) = (motorMixer_t){ 1.0f, -1.0f, -0.414178f, -1.0f };    // MIDFRONT_R
    *customMotorMixer(5) = (motorMixer_t){ 1.0f,  1.0f, -0.414178f,  1.0f };    // MIDFRONT_L
    *customMotorMixer(6) = (motorMixer_t){ 1.0f, -1.0f,  0.414178f,  1.0f };    // MIDREAR_R
    *customMotorMixer(7) = (motorMixer_t){ 1.0f,  1.0f,  0.414178f, -1.0f };    // MIDREAR_L
#endif

    // copy first profile into remaining profile
    PG_FOREACH_PROFILE(reg) {
        for (int i = 1; i < MAX_PROFILE_COUNT; i++) {
            memcpy(reg->address + i * pgSize(reg), reg->address, pgSize(reg));
        }
    }
    for (int i = 1; i < MAX_PROFILE_COUNT; i++) {
        configureRateProfileSelection(i, i % MAX_CONTROL_RATE_PROFILE_COUNT);
    }
}
예제 #13
0
// Default settings
static void resetConf(void)
{
    uint8_t i;
    const int8_t default_align[3][3] = { /* GYRO */ { 0, 0, 0 }, /* ACC */ { 0, 0, 0 }, /* MAG */ { -2, -3, 1 } };
    memset(&cfg, 0, sizeof(config_t));

    cfg.version = EEPROM_CONF_VERSION;
    cfg.mixerConfiguration = MULTITYPE_QUADX;
    featureClearAll();
//    featureSet(FEATURE_VBAT);
    featureSet(FEATURE_PPM);
//    featureSet(FEATURE_FAILSAFE);
//    featureSet(FEATURE_LCD);
//    featureSet(FEATURE_GPS);
//    featureSet(FEATURE_PASS);                   // Just pass Throttlechannel
//    featureSet(FEATURE_SONAR);

    cfg.P8[ROLL]                  = 35;         // 40
    cfg.I8[ROLL]                  = 20;
    cfg.D8[ROLL]                  = 30;

    cfg.P8[PITCH]                 = 35;         // 40
    cfg.I8[PITCH]                 = 20;
    cfg.D8[PITCH]                 = 30;

    cfg.P8[YAW]                   = 60;         // 70
    cfg.I8[YAW]                   = 45;

    cfg.P8[PIDALT]                = 100;
    cfg.I8[PIDALT]                = 30;
    cfg.D8[PIDALT]                = 80;

    cfg.P8[PIDPOS]                = 10;         // FIND YOUR VALUE
    cfg.I8[PIDPOS]                =  0;         // NOT USED
    cfg.D8[PIDPOS]                =  0;         // NOT USED

    cfg.P8[PIDPOSR]               = 50;         // FIND YOUR VALUE                    // Controls the speed part with my PH logic
    cfg.I8[PIDPOSR]               =  0;         // 25;  // DANGER "I" may lead to circeling   // Controls the speed part with my PH logic
    cfg.D8[PIDPOSR]               = 40;         // FIND YOUR VALUE                    // Controls the speed part with my PH logic

    cfg.P8[PIDNAVR]               = 15;         // 14 More ?
    cfg.I8[PIDNAVR]               =  0;         // NAV_I * 100;                       // Scaling/Purpose unchanged
    cfg.D8[PIDNAVR]               =  0;         // NAV_D * 1000;                      // Scaling/Purpose unchanged

//    cfg.P8[PIDPOS]                = 11;         // APM PH Stock values
//    cfg.I8[PIDPOS]                = 0;
//    cfg.D8[PIDPOS]                = 0;

//    cfg.P8[PIDPOSR]               = 20;         // POSHOLD_RATE_P * 10;
//    cfg.I8[PIDPOSR]               = 8;          // POSHOLD_RATE_I * 100;
//    cfg.D8[PIDPOSR]               = 45;         // POSHOLD_RATE_D * 1000;

//    cfg.P8[PIDNAVR]               = 14;         // NAV_P * 10;
//    cfg.I8[PIDNAVR]               = 20;         // NAV_I * 100;
//    cfg.D8[PIDNAVR]               = 80;         // NAV_D * 1000;

    cfg.P8[PIDLEVEL]              = 60;         // 70
    cfg.I8[PIDLEVEL]              = 10;
    cfg.D8[PIDLEVEL]              = 50;

    cfg.P8[PIDMAG]                = 80;         // cfg.P8[PIDVEL] = 0;// cfg.I8[PIDVEL] = 0;// cfg.D8[PIDVEL] = 0;

    cfg.rcRate8                   = 100;
    cfg.rcExpo8                   = 80;         // cfg.rollPitchRate = 0;// cfg.yawRate = 0;// cfg.dynThrPID = 0;
    cfg.thrMid8                   = 50;
    // cfg.thrExpo8 = 0;//for (i = 0; i < CHECKBOXITEMS; i++)//cfg.activate[i] = 0;
    // cfg.angleTrim[0] = 0;// cfg.angleTrim[1] = 0;// cfg.accZero[0] = 0;// cfg.accZero[1] = 0;
    // cfg.accZero[2] = 0;// cfg.mag_declination = 0;    // For example, -6deg 37min, = -637 Japan, format is [sign]dddmm (degreesminutes) default is zero.
    memcpy(&cfg.align, default_align, sizeof(cfg.align));

//    cfg.mag_declination           = 0;          // For example, -6deg 37min, = -637 Japan, format is [sign]dddmm (degreesminutes) default is zero.
    cfg.mag_declination           = 107;        // Crashpilot //cfg.acc_hardware = ACC_DEFAULT;// default/autodetect
    cfg.mag_oldcalib              = 0;          // 1 = old hard iron calibration // 0 = extended calibration (better)
    cfg.mag_oldctime              = 1;          // 1 - 5 Time in MINUTES for old calibration. Use this together with mag_oldcalib = 1 if you have a monster of a copter
    cfg.acc_hardware              = 2;          // Crashpilot MPU6050
    cfg.acc_lpf_factor            = 100;	      // changed 27.11.2012
    cfg.acc_ins_lpf               = 10;         // General LPF for all INS stuff

    cfg.looptime                  = 3000;	      // changed 27.11.2012 //    cfg.acc_lpf_factor = 4;
    cfg.mainpidctrl               = 1;          // 1 = OriginalMwiiPid pimped by me, 2 = New mwii controller (experimental, float pimped + pt1)
    cfg.mainpt1cut                = 15;         // (0-50Hz) 0 Disables pt1element. Cuf Off Frequency for pt1 element D term in Hz of main Pid controller
    cfg.newpidimax                = 256;        // [10-65000) 256 Default. Imax of new Pidcontroller
    cfg.gpspt1cut                 = 10;         // (1-50Hz) Cuf Off Frequency for D term in Hz of GPS Pid controller 
    cfg.gyro_cmpf_factor          = 1000;       // (10-1000) 400 default. Now 1000. The higher, the more weight gets the gyro and the lower is the correction with Acc data.
    cfg.gyro_cmpfm_factor         = 1000;       // (10-2000) 200 default for 10Hz. Now 1000 for 70Hz seems ok. Gyro/Magnetometer Complement. Greater Value means more filter on mag/delay
    
    cfg.gyro_lpf                  = 42;         // Possible values 256 188 98 42 20 10 (HZ)

    // Baro
    cfg.accz_vel_cf               = 0.985f;     // Crashpilot: Value for complementary filter accz and barovelocity
    cfg.accz_alt_cf               = 0.940f;     // Crashpilot: Value for complementary filter accz and altitude
    cfg.baro_lag                  = 0.3f;       // Lag of Baro/Althold stuff in general, makes stop in hightchange snappier
    cfg.barodownscale             = 0.7f;       // Scale downmovement down (because copter drops faster than rising)

    // Autoland
    cfg.al_barolr                 = 75;         // Temporary value "64" increase to increase Landingspeed
    cfg.al_snrlr                  = 75;         // You can specify different landingfactor here on sonar contact, because sonar land maybe too fast when snr_cf is high
    cfg.al_lndthr                 = 0;          // This is the absolute throttle that kicks off the "has landed timer" if it is too low cfg.minthrottle is taken.
    cfg.al_debounce               = 5;          // (0-20%) 0 Disables. Defines a Throttlelimiter on Autoland. Percentage defines the maximum deviation of assumed hoverthrottle during Autoland
    cfg.al_tobaro                 = 2000;       // Timeout in ms (100 - 5000) before shutoff on autoland. "al_lndthr" must be undershot for that timeperiod
    cfg.al_tosnr                  = 1000;       // Timeout in ms (100 - 5000) If sonar aided land is wanted (snr_land = 1) you can choose a different timeout here

    cfg.baro_debug                = 0;          // Crashpilot: 1 = Debug Barovalues //cfg.baro_noise_lpf = 0.6f;// Crashpilot: Not used anymore//cfg.baro_cf = 0.985f;// Crashpilot: Not used anymore
    cfg.moron_threshold           = 32;
    cfg.gyro_smoothing_factor     = 0x00141403; // default factors of 20, 20, 3 for R/P/Y
    cfg.vbatscale                 = 110;
    cfg.vbatmaxcellvoltage        = 43;
    cfg.vbatmincellvoltage        = 33;
    cfg.power_adc_channel         = 0;

    // Radio
    parseRcChannels("AETR1234");
    cfg.deadband                  = 15;         // Crashpilot: A little deadband will not harm our crappy RC
    cfg.yawdeadband               = 15;         // Crashpilot: A little deadband will not harm our crappy RC
    cfg.alt_hold_throttle_neutral = 50;         // Crashpilot: A little deadband will not harm our crappy RC
    cfg.gps_adddb                 = 5;          // Additional Deadband for all GPS functions;

    // cfg.spektrum_hires = 0;
    cfg.midrc                     = 1500;
    cfg.mincheck                  = 1100;
    cfg.maxcheck                  = 1900;
    cfg.retarded_arm              = 0;          // disable arm/disarm on roll left/right
    cfg.auxChannels               = 4;          // [4 - 10] cGiesen: Default = 4, then like the standard!
    cfg.killswitchtime            = 0;          // Time in ms when your arm switch becomes a Killswitch, 0 disables the Killswitch, can not be used together with FEATURE_INFLIGHT_ACC_CAL

    // Motor/ESC/Servo
    cfg.minthrottle               = 1150;       // ORIG
//    cfg.minthrottle               = 1100;
    cfg.maxthrottle               = 1950;
    cfg.passmotor                 = 0;          // Crashpilot: Only used with feature pass. If 0 = all Motors, otherwise specific Motor
    cfg.mincommand                = 1000;
    cfg.motor_pwm_rate            = 400;
    cfg.servo_pwm_rate            = 50;

    // servos
    cfg.yaw_direction             = 1;
    cfg.tri_yaw_middle            = 1500;
    cfg.tri_yaw_min               = 1020;
    cfg.tri_yaw_max               = 2000;

    // flying wing
    cfg.wing_left_min             = 1020;
    cfg.wing_left_mid             = 1500;
    cfg.wing_left_max             = 2000;
    cfg.wing_right_min            = 1020;
    cfg.wing_right_mid            = 1500;
    cfg.wing_right_max            = 2000;
    cfg.pitch_direction_l         = 1;
    cfg.pitch_direction_r         = -1;
    cfg.roll_direction_l          = 1;
    cfg.roll_direction_r          = 1;

    // gimbal
    cfg.gimbal_pitch_gain         = 10;
    cfg.gimbal_roll_gain          = 10;
    cfg.gimbal_flags              = GIMBAL_NORMAL;
    cfg.gimbal_pitch_min          = 1020;
    cfg.gimbal_pitch_max          = 2000;
    cfg.gimbal_pitch_mid          = 1500;
    cfg.gimbal_roll_min           = 1020;
    cfg.gimbal_roll_max           = 2000;
    cfg.gimbal_roll_mid           = 1500;

    // gps/nav
    cfg.gps_type                  = 1;          // GPS_NMEA = 0, GPS_UBLOX = 1, GPS_MTK16 = 2, GPS_MTK19 = 3, GPS_UBLOX_DUMB = 4
    cfg.gps_baudrate              = 115200;     //38400; // Changed 8/6/13 to 115200;
//    cfg.gps_baudrate              = 38400;      //38400; // Changed 8/6/13 to 115200;
//    cfg.gps_ins_vel               = 0.72f;      // Crashpilot GPS INS The LOWER the value the closer to gps speed // Dont go to high here
    cfg.gps_ins_vel               = 0.6f;       // Crashpilot GPS INS The LOWER the value the closer to gps speed // Dont go to high here
    cfg.gps_ins_mdl               = 1;          // NOTE: KEEP THIS TO "1" FOR NOW because other models work like shit currently. GPS ins model. 1 = Based on lat/lon, 2 = based on Groundcourse & speed,(3 = based on ublx velned deleted)
    cfg.gps_lag                   = 2000;       // GPS Lag in ms
    cfg.gps_phase                 = 0;          // +- 30 Degree Make a phaseshift of GPS output for whatever reason you might want that (frametype etc)
    cfg.gps_ph_minsat             = 6;          // Minimal Satcount for PH, PH on RTL is still done with 5Sats or more
    cfg.gps_ph_settlespeed        = 10;         // 1 - 200 cm/s PH settlespeed in cm/s
    cfg.gps_ph_brakemaxangle      = 10;         // 1 - 45 Degree Maximal 5 Degree Overspeedbrake
    cfg.gps_ph_minbrakepercent    = 50;         // 1 - 99% minimal percent of "brakemaxangle" left over for braking. Example brakemaxangle = 6 so 50 Percent is 3..
    cfg.gps_ph_brkacc             = 40;         // [1 - 500] Is the assumed negative braking acceleration in cm/(s*s) of copter. Value is positive though. It will be a timeout. The lower the Value the longe the Timeout
    cfg.gps_ph_abstub             = 100;        // 0 - 1000cm (300 Dfault, 0 disables) Defines the "bath tub" around current absolute PH Position, where PosP is diminished, reaction gets harder on tubs edge and then goes on linear
    cfg.gps_maxangle              = 25;         // 10 - 45 Degree Maximal over all GPS bank angle
    cfg.gps_wp_radius             = 150;
//    cfg.gps_rtl_minhight          = 20;         // (0 - 200) Minimal RTL hight in m, 0 disables feature
	  cfg.gps_rtl_minhight          = 0;          // (0 - 200) Minimal RTL hight in m, 0 disables feature
    cfg.gps_rtl_mindist           = 0;          // 0 Disables. Minimal distance for RTL in m, otherwise it will just autoland, prevent Failsafe jump in your face, when arming copter and turning off TX
    cfg.gps_rtl_flyaway           = 0;          // 0 Disables. If during RTL the distance increases beyond this value (in meters relative to RTL activation point), something is wrong, autoland
    cfg.gps_yaw                   = 30;         // Thats the MAG P during GPS functions, substitute for "cfg.P8[PIDMAG]"
    cfg.nav_rtl_lastturn          = 1;          // 1 = when copter gets to home position it rotates it's head to takeoff direction independend of nav_controls_heading
//    cfg.nav_slew_rate             = 30;         // was 30 and 50 before
    cfg.nav_slew_rate             = 20;         // was 30 and 50 before
    cfg.nav_tail_first            = 0;          // 1 = Copter comes back with ass first (only works with nav_controls_heading = 1)
    cfg.nav_controls_heading      = 0;          // 1 = Nav controls YAW during WP ONLY
//    cfg.nav_controls_heading      = 1;          // 1 = Nav controls YAW during WP ONLY
    cfg.nav_speed_min             = 100;        // 10 - 200 cm/s don't set higher than nav_speed_max! That dumbness is not covered.
    cfg.nav_speed_max             = 350;        // 50 - 2000 cm/s don't set lower than nav_speed_min! That dumbness is not covered.
    cfg.nav_approachdiv           = 3;          // 2 - 10 This is the divisor for approach speed for wp_distance. Example: 400cm / 3 = 133cm/s if below nav_speed_min it will be adjusted
    cfg.nav_tiltcomp              = 20;         // 0 - 100 (20 TestDefault) Only arducopter really knows. Dfault was 54. This is some kind of a hack of them to reach actual nav_speed_max. 54 was Dfault, 0 disables
    cfg.nav_ctrkgain              = 0.5f;       // 0 - 10.0 (0.5 TestDefault) (Floatvariable) That is the "Crosstrackgain" APM Dfault is "1". "0" disables

    // Failsafe Variables
    cfg.failsafe_delay            = 10;         // in 0.1s (10 = 1sec)
    cfg.failsafe_off_delay        = 200;        // in 0.1s (200 = 20sec)
    cfg.failsafe_throttle         = 1200;       // decent Dfault which should always be below hover throttle for people.
    cfg.failsafe_deadpilot        = 0;		      // DONT USE, EXPERIMENTAL Time in sec when FS is engaged after idle on THR/YAW/ROLL/PITCH, 0 disables max 250
    cfg.failsafe_justph           = 0;          // Does just PH&Autoland an not RTL, use this in difficult areas with many obstacles to avoid RTL crash into something
    cfg.failsafe_ignoreSNR        = 1;          // When snr_land is set to 1, it is possible to ignore that on Failsafe, because FS over a tree could turn off copter

    // serial (USART1) baudrate
    cfg.serial_baudrate           = 115200;
    cfg.tele_prot                 = 0;          // Protocol ONLY used when Armed including Baudchange if necessary. 0 (Dfault)=Keep Multiwii @CurrentUSB Baud, 1=Frsky @9600Baud, 2=Mavlink @CurrentUSB Baud, 3=Mavlink @57KBaud (like stock minimOSD wants it)

    // LED Stuff
    cfg.LED_invert                = 0;          // Crashpilot: Inversion of LED 0&1 Partly implemented because Bootup is not affected
    cfg.LED_Type                  = 1;		      // 1=MWCRGB / 2=MONO_LED / 3=LEDRing
    cfg.LED_Pinout                = 1;		      // rc6
    cfg.LED_ControlChannel        = 8;		      // AUX4 (Channel 8)
    cfg.LED_Armed                 = 0;		      // 0 = Show LED only if armed, 1 = always show LED
    cfg.LED_Pattern1			        = 1300; 		  // 32bit bit pattern to have flickering led patterns / the pattern for MWCRGB 1000-2000
    cfg.LED_Pattern2			        = 1800; 		  // 32bit bit pattern to have flickering led patterns / the pattern for MWCRGB 1000-2000
    cfg.LED_Pattern3			        = 1900; 		  // 32bit bit pattern to have flickering led patterns / the pattern for MWCRGB 1000-2000
    cfg.LED_Toggle_Delay1         = 0x08;       // slow down LED_Pattern
    cfg.LED_Toggle_Delay2         = 0x08;       // slow down LED_Pattern
    cfg.LED_Toggle_Delay3         = 0x08;       // slow down LED_Pattern

    // SONAR

    // SOME INFO ON SONAR:
    // PWM56 are 5V resistant, RC78 only tolerate 3.3V(!!) so add a 1K Ohms resistor!!!
    // Note: You will never see the maximum possible sonar range in a copter, so go for the half of it (or less?)
    //
    // Connection possibilities depending on Receivertype:
    // PPSUM: RC78 possible, PWM56 possible (on max. quadcopters, see below)
    // Normal RX: Just Connection on Motorchannel 5&6 (PWM56) is possible.
    // The PWM56 sonar connection option is only available in setups with max motors 4, otherwise sonar is not initialized.
    //
    // HC-SR04:
    // Operation Voltage: 5V (!! Use PWM56 or 1K resistor !!)
    // Range: 2cm - 400cm
    // Angle: 15 Degrees (Test out for yourself: cfg.snr_tilt = X)
    //
    // Maxbotics in general
    // Operation Voltage: (some 2.5V)3.3V - 5V ((!! Use PWM56 or resistor with 5V !!)
    // Only wire the Maxbotics for PWM output (more precise anyway), not the analog etc. modes, just wire echopin (normally pin 2)
    // Range: 20cm(!) - 765cm (some >1000cm), MaxTiltAngle is not specified, depending on Model
    // Tested on MB1200 XL-MaxSonar-EZ0
    //
    // GENERAL WARNING: DON'T SET snr_min TOO LOW, OTHERWISE THE WRONG SONARVALUE WILL BE TAKEN AS REAL MEASUREMENT!!
    // I implemented some checks to prevent that user error, but still keep that in mind.
    // Min/Max are checked and changed if they are too stupid for your sonar. So if you suddenly see other values, thats not an eeprom error or so.
    // MAXBOTICS: SET snr_min to at least 25! I check this in sensors and change the value, if needed.
    // NOTE: I limited Maxbotics to 7 meters in the code, knowing that some types will do >10m, if you have one of them 7m is still the limit for you.
    // HC-SR04:   SET snr_min to at least 5 ! I check this in sensors and change the value, if needed.
    // DaddyWalross Sonar: I DON'T KNOW! But it uses HC-SR04 so i apply the same limits (5cm-400cm) to its output
    // NOTE: Sonar is def. not a must - have. But nice to have.
    cfg.snr_type                  = 3;          // 0 = PWM56 HC-SR04, 1 = RC78 HC-SR04, 2 = I2C (DaddyWalross), 3 = MBPWM56, 4 = MBRC78
    cfg.snr_min                   = 25;         // Valid Sonar minimal range in cm (5-200) see warning above
    cfg.snr_max                   = 200;        // Valid Sonar maximal range in cm (50-700)
    cfg.snr_debug                 = 0;          // 1 Sends Sonardata (within defined range and tilt) to debug[0] and tiltvalue to debug[1], debug[0] will be -1 if out of range/tilt. debug[2] contains raw sonaralt, like before
    cfg.snr_tilt                  = 18;         // Somehow copter tiltrange in degrees (Not exactly but good enough. Value * 0.9 = realtilt) in wich Sonar is possible
    cfg.snr_cf                    = 0.7f;       // The bigger, the more Sonarinfluence, makes switch between Baro/Sonar smoother and defines baroinfluence when sonarcontact. 1.0f just takes Sonar, if contact (otherwise baro)
    cfg.snr_diff                  = 0;          // 0 disables that check. Range (0-200) Maximal allowed difference in cm between sonar readouts (100ms rate and snr_diff = 50 means max 5m/s)
    cfg.snr_land                  = 1;          // Aided Sonar - landing, by setting upper throttle limit to current throttle. - Beware of Trees!! Can be disabled for Failsafe with failsafe_ignoreSNR = 1

    // LOGGING
    cfg.floppy_mode               = FD_MODE_GPSLOGGER; // Usagemode of free Space. 1 = GPS Logger
    cfg.FDUsedDatasets            = 0;          // Default no Datasets stored
    cfg.stat_clear                = 1;          // This will clear the stats between flights, or you can set to 0 and treasue overallstats, but you have to write manually eeprom or have logging enabled
    cfg.sens_1G                   = 1;          // Just feed a dummy "1" to avoid div by zero
    ClearStats();
    // custom mixer. clear by Dfaults.
    for (i = 0; i < MAX_MOTORS; i++) cfg.customMixer[i].throttle = 0.0f;
    writeParams(0);
}
예제 #14
0
// Default settings
static void resetConf(void)
{
    int i;
    int8_t servoRates[8] = { 30, 30, 100, 100, 100, 100, 100, 100 };

    // Clear all configuration
    memset(&masterConfig, 0, sizeof(master_t));
    memset(&currentProfile, 0, sizeof(profile_t));

    masterConfig.version = EEPROM_CONF_VERSION;
    masterConfig.mixerConfiguration = MULTITYPE_QUADX;
    featureClearAll();
    featureSet(FEATURE_VBAT);

    // global settings
    masterConfig.current_profile_index = 0;     // default profile
    masterConfig.gyro_cmpf_factor = 600;        // default MWC
    masterConfig.gyro_cmpfm_factor = 250;       // default MWC
    masterConfig.gyro_lpf = 42;                 // supported by all gyro drivers now. In case of ST gyro, will default to 32Hz instead

    resetAccelerometerTrims(&masterConfig.accZero);

    resetSensorAlignment(&masterConfig.sensorAlignmentConfig);

    masterConfig.boardAlignment.rollDegrees = 0;
    masterConfig.boardAlignment.pitchDegrees = 0;
    masterConfig.boardAlignment.yawDegrees = 0;
    masterConfig.acc_hardware = ACC_DEFAULT;     // default/autodetect
    masterConfig.max_angle_inclination = 500;    // 50 degrees
    masterConfig.yaw_control_direction = 1;
    masterConfig.gyroConfig.gyroMovementCalibrationThreshold = 32;

    masterConfig.batteryConfig.vbatscale = 110;
    masterConfig.batteryConfig.vbatmaxcellvoltage = 43;
    masterConfig.batteryConfig.vbatmincellvoltage = 33;
    masterConfig.batteryConfig.currentMeterOffset = 0;
    masterConfig.batteryConfig.currentMeterScale = 400; // for Allegro ACS758LCB-100U (40mV/A)

    resetTelemetryConfig(&masterConfig.telemetryConfig);

    masterConfig.rxConfig.serialrx_provider = 0;
    masterConfig.rxConfig.midrc = 1500;
    masterConfig.rxConfig.mincheck = 1100;
    masterConfig.rxConfig.maxcheck = 1900;
    masterConfig.rxConfig.rssi_channel = 0;

    masterConfig.retarded_arm = 0;              // disable arm/disarm on roll left/right
    masterConfig.airplaneConfig.flaps_speed = 0;
    masterConfig.fixedwing_althold_dir = 1;

    // Motor/ESC/Servo
    resetEscAndServoConfig(&masterConfig.escAndServoConfig);
    resetFlight3DConfig(&masterConfig.flight3DConfig);
    masterConfig.motor_pwm_rate = 400;
    masterConfig.servo_pwm_rate = 50;

    // gps/nav stuff
    masterConfig.gpsConfig.provider = GPS_NMEA;
    masterConfig.gpsConfig.sbasMode = SBAS_AUTO;

    resetSerialConfig(&masterConfig.serialConfig);

    masterConfig.looptime = 3500;
    masterConfig.emf_avoidance = 0;

    currentProfile.pidController = 0;
    resetPidProfile(&currentProfile.pidProfile);

    currentProfile.controlRateConfig.rcRate8 = 90;
    currentProfile.controlRateConfig.rcExpo8 = 65;
    currentProfile.controlRateConfig.rollPitchRate = 0;
    currentProfile.controlRateConfig.yawRate = 0;
    currentProfile.dynThrPID = 0;
    currentProfile.tpa_breakpoint = 1500;
    currentProfile.controlRateConfig.thrMid8 = 50;
    currentProfile.controlRateConfig.thrExpo8 = 0;

    // for (i = 0; i < CHECKBOXITEMS; i++)
    //     cfg.activate[i] = 0;

    resetRollAndPitchTrims(&currentProfile.accelerometerTrims);

    currentProfile.mag_declination = 0;
    currentProfile.acc_lpf_factor = 4;
    currentProfile.accDeadband.xy = 40;
    currentProfile.accDeadband.z = 40;

    resetBarometerConfig(&currentProfile.barometerConfig);

    currentProfile.acc_unarmedcal = 1;

    // Radio
    parseRcChannels("AETR1234", &masterConfig.rxConfig);
    currentProfile.deadband = 0;
    currentProfile.yaw_deadband = 0;
    currentProfile.alt_hold_deadband = 40;
    currentProfile.alt_hold_fast_change = 1;
    currentProfile.throttle_correction_value = 0;      // could 10 with althold or 40 for fpv
    currentProfile.throttle_correction_angle = 800;    // could be 80.0 deg with atlhold or 45.0 for fpv

    // Failsafe Variables
    currentProfile.failsafeConfig.failsafe_delay = 10;              // 1sec
    currentProfile.failsafeConfig.failsafe_off_delay = 200;         // 20sec
    currentProfile.failsafeConfig.failsafe_throttle = 1200;         // decent default which should always be below hover throttle for people.
    currentProfile.failsafeConfig.failsafe_min_usec = 985;          // any of first 4 channels below this value will trigger failsafe
    currentProfile.failsafeConfig.failsafe_max_usec = 2115;         // any of first 4 channels above this value will trigger failsafe

    // servos
    for (i = 0; i < 8; i++) {
        currentProfile.servoConf[i].min = DEFAULT_SERVO_MIN;
        currentProfile.servoConf[i].max = DEFAULT_SERVO_MAX;
        currentProfile.servoConf[i].middle = DEFAULT_SERVO_MIDDLE;
        currentProfile.servoConf[i].rate = servoRates[i];
        currentProfile.servoConf[i].forwardFromChannel = CHANNEL_FORWARDING_DISABLED;
    }

    currentProfile.mixerConfig.yaw_direction = 1;
    currentProfile.mixerConfig.tri_unarmed_servo = 1;

    // gimbal
    currentProfile.gimbalConfig.gimbal_flags = GIMBAL_NORMAL;

    resetGpsProfile(&currentProfile.gpsProfile);

    // custom mixer. clear by defaults.
    for (i = 0; i < MAX_SUPPORTED_MOTORS; i++)
        masterConfig.customMixer[i].throttle = 0.0f;

    // copy default config into all 3 profiles
    for (i = 0; i < 3; i++)
        memcpy(&masterConfig.profile[i], &currentProfile, sizeof(profile_t));
예제 #15
0
// Default settings
static void resetConf(void)
{
    int i;
    int8_t servoRates[8] = { 30, 30, 100, 100, 100, 100, 100, 100 };

    // Clear all configuration
    memset(&mcfg, 0, sizeof(master_t));
    memset(&cfg, 0, sizeof(config_t));

    mcfg.version = EEPROM_CONF_VERSION;
    mcfg.mixerConfiguration = MULTITYPE_QUADX;
    featureClearAll();
    featureSet(FEATURE_VBAT);

    // global settings
    mcfg.current_profile = 0;       // default profile
    mcfg.gyro_cmpf_factor = 600;    // default MWC
    mcfg.gyro_cmpfm_factor = 250;   // default MWC
    mcfg.gyro_lpf = 42;             // supported by all gyro drivers now. In case of ST gyro, will default to 32Hz instead
    mcfg.accZero[0] = 0;
    mcfg.accZero[1] = 0;
    mcfg.accZero[2] = 0;
    mcfg.gyro_align = ALIGN_DEFAULT;
    mcfg.acc_align = ALIGN_DEFAULT;
    mcfg.mag_align = ALIGN_DEFAULT;
    mcfg.board_align_roll = 0;
    mcfg.board_align_pitch = 0;
    mcfg.board_align_yaw = 0;
    mcfg.acc_hardware = ACC_DEFAULT;     // default/autodetect
    mcfg.max_angle_inclination = 500;    // 50 degrees
    mcfg.yaw_control_direction = 1;
    mcfg.moron_threshold = 32;
    mcfg.vbatscale = 110;
    mcfg.vbatmaxcellvoltage = 43;
    mcfg.vbatmincellvoltage = 33;
    mcfg.power_adc_channel = 0;
    mcfg.serialrx_type = 0;
    mcfg.telemetry_softserial = 0;
    mcfg.telemetry_switch = 0;
    mcfg.midrc = 1500;
    mcfg.mincheck = 1100;
    mcfg.maxcheck = 1900;
    mcfg.retarded_arm = 0;       // disable arm/disarm on roll left/right
    mcfg.flaps_speed = 0;
    mcfg.fixedwing_althold_dir = 1;
    // Motor/ESC/Servo
    mcfg.minthrottle = 1150;
    mcfg.maxthrottle = 1850;
    mcfg.mincommand = 1000;
    mcfg.deadband3d_low = 1406;
    mcfg.deadband3d_high = 1514;
    mcfg.neutral3d = 1460;
    mcfg.deadband3d_throttle = 50;
    mcfg.motor_pwm_rate = 400;
    mcfg.servo_pwm_rate = 50;
    // gps/nav stuff
    mcfg.gps_type = GPS_NMEA;
    mcfg.gps_baudrate = 0;
    // serial (USART1) baudrate
    mcfg.serial_baudrate = 115200;
    mcfg.softserial_baudrate = 19200;
    mcfg.softserial_inverted = 0;
    mcfg.looptime = 3500;
    mcfg.rssi_aux_channel = 0;

    cfg.pidController = 0;
    cfg.P8[ROLL] = 40;
    cfg.I8[ROLL] = 30;
    cfg.D8[ROLL] = 23;
    cfg.P8[PITCH] = 40;
    cfg.I8[PITCH] = 30;
    cfg.D8[PITCH] = 23;
    cfg.P8[YAW] = 85;
    cfg.I8[YAW] = 45;
    cfg.D8[YAW] = 0;
    cfg.P8[PIDALT] = 50;
    cfg.I8[PIDALT] = 0;
    cfg.D8[PIDALT] = 0;
    cfg.P8[PIDPOS] = 11; // POSHOLD_P * 100;
    cfg.I8[PIDPOS] = 0; // POSHOLD_I * 100;
    cfg.D8[PIDPOS] = 0;
    cfg.P8[PIDPOSR] = 20; // POSHOLD_RATE_P * 10;
    cfg.I8[PIDPOSR] = 8; // POSHOLD_RATE_I * 100;
    cfg.D8[PIDPOSR] = 45; // POSHOLD_RATE_D * 1000;
    cfg.P8[PIDNAVR] = 14; // NAV_P * 10;
    cfg.I8[PIDNAVR] = 20; // NAV_I * 100;
    cfg.D8[PIDNAVR] = 80; // NAV_D * 1000;
    cfg.P8[PIDLEVEL] = 90;
    cfg.I8[PIDLEVEL] = 10;
    cfg.D8[PIDLEVEL] = 100;
    cfg.P8[PIDMAG] = 40;
    cfg.P8[PIDVEL] = 120;
    cfg.I8[PIDVEL] = 45;
    cfg.D8[PIDVEL] = 1;
    cfg.rcRate8 = 90;
    cfg.rcExpo8 = 65;
    cfg.rollPitchRate = 0;
    cfg.yawRate = 0;
    cfg.dynThrPID = 0;
    cfg.thrMid8 = 50;
    cfg.thrExpo8 = 0;
    // for (i = 0; i < CHECKBOXITEMS; i++)
    //     cfg.activate[i] = 0;
    cfg.angleTrim[0] = 0;
    cfg.angleTrim[1] = 0;
    cfg.mag_declination = 0;    // For example, -6deg 37min, = -637 Japan, format is [sign]dddmm (degreesminutes) default is zero.
    cfg.acc_lpf_factor = 4;
    cfg.accz_deadband = 40;
    cfg.accxy_deadband = 40;
    cfg.baro_tab_size = 21;
    cfg.baro_noise_lpf = 0.6f;
    cfg.baro_cf_vel = 0.985f;
    cfg.baro_cf_alt = 0.965f;
    cfg.acc_unarmedcal = 1;

    // Radio
    parseRcChannels("AETR1234");
    cfg.deadband = 0;
    cfg.yawdeadband = 0;
    cfg.alt_hold_throttle_neutral = 40;
    cfg.alt_hold_fast_change = 1;
    cfg.throttle_angle_correction = 0;      // could be 40

    // Failsafe Variables
    cfg.failsafe_delay = 10;                // 1sec
    cfg.failsafe_off_delay = 200;           // 20sec
    cfg.failsafe_throttle = 1200;           // decent default which should always be below hover throttle for people.
    cfg.failsafe_detect_threshold = 985;    // any of first 4 channels below this value will trigger failsafe

    // servos
    for (i = 0; i < 8; i++) {
        cfg.servoConf[i].min = 1020;
        cfg.servoConf[i].max = 2000;
        cfg.servoConf[i].middle = 1500;
        cfg.servoConf[i].rate = servoRates[i];
    }

    cfg.yaw_direction = 1;
    cfg.tri_unarmed_servo = 1;

    // gimbal
    cfg.gimbal_flags = GIMBAL_NORMAL;

    // gps/nav stuff
    cfg.gps_wp_radius = 200;
    cfg.gps_lpf = 20;
    cfg.nav_slew_rate = 30;
    cfg.nav_controls_heading = 1;
    cfg.nav_speed_min = 100;
    cfg.nav_speed_max = 300;
    cfg.ap_mode = 40;

    // custom mixer. clear by defaults.
    for (i = 0; i < MAX_MOTORS; i++)
        mcfg.customMixer[i].throttle = 0.0f;

    // copy default config into all 3 profiles
    for (i = 0; i < 3; i++)
        memcpy(&mcfg.profile[i], &cfg, sizeof(config_t));
}
예제 #16
0
// Default settings
STATIC_UNIT_TESTED void resetConf(void)
{
    int i;

    // Clear all configuration
    memset(&masterConfig, 0, sizeof(master_t));
    setProfile(0);
    setControlRateProfile(0);

    masterConfig.version = EEPROM_CONF_VERSION;
    masterConfig.mixerMode = MIXER_QUADX;
    featureClearAll();
#if defined(CJMCU) || defined(SPARKY) || defined(COLIBRI_RACE) || defined(MOTOLAB) || defined(SPRACINGF3MINI) || defined(LUX_RACE)
    featureSet(FEATURE_RX_PPM);
#endif

//#if defined(SPRACINGF3MINI)
//    featureSet(FEATURE_DISPLAY);
//#endif

#ifdef BOARD_HAS_VOLTAGE_DIVIDER
    // only enable the VBAT feature by default if the board has a voltage divider otherwise
    // the user may see incorrect readings and unexpected issues with pin mappings may occur.
    featureSet(FEATURE_VBAT);
#endif

    featureSet(FEATURE_FAILSAFE);

    // global settings
    masterConfig.dcm_kp = 2500;                // 1.0 * 10000
    masterConfig.gyro_lpf = 1;                 // supported by all gyro drivers now. In case of ST gyro, will default to 32Hz instead
    masterConfig.soft_gyro_lpf_hz = 60;        // Software based lpf filter for gyro

    masterConfig.max_angle_inclination = 500;    // 50 degrees
    masterConfig.yaw_control_direction = 1;
    masterConfig.gyroConfig.gyroMovementCalibrationThreshold = 32;

    resetBatteryConfig(&masterConfig.batteryConfig);

#ifdef TELEMETRY
    masterConfig.telemetryConfig.hottAlarmSoundInterval = 5;
#endif

    masterConfig.rxConfig.sbus_inversion = 1;
    masterConfig.rxConfig.midrc = 1500;
    masterConfig.rxConfig.mincheck = 1100;
    masterConfig.rxConfig.maxcheck = 1900;
    masterConfig.rxConfig.rx_min_usec = 885;          // any of first 4 channels below this value will trigger rx loss detection
    masterConfig.rxConfig.rx_max_usec = 2115;         // any of first 4 channels above this value will trigger rx loss detection

    for (i = 0; i < MAX_SUPPORTED_RC_CHANNEL_COUNT; i++) {
        rxFailsafeChannelConfiguration_t *channelFailsafeConfiguration = &masterConfig.rxConfig.failsafe_channel_configurations[i];
        channelFailsafeConfiguration->mode = (i < NON_AUX_CHANNEL_COUNT) ? RX_FAILSAFE_MODE_AUTO : RX_FAILSAFE_MODE_HOLD;
        channelFailsafeConfiguration->step = (i == THROTTLE) ? CHANNEL_VALUE_TO_RXFAIL_STEP(masterConfig.rxConfig.rx_min_usec) : CHANNEL_VALUE_TO_RXFAIL_STEP(masterConfig.rxConfig.midrc);
    }

    masterConfig.rxConfig.rssi_scale = RSSI_SCALE_DEFAULT;

    resetAllRxChannelRangeConfigurations(masterConfig.rxConfig.channelRanges);

    masterConfig.disarm_kill_switch = 1;
    masterConfig.auto_disarm_delay = 5;
    masterConfig.small_angle = 25;

    resetMixerConfig(&masterConfig.mixerConfig);

    masterConfig.airplaneConfig.fixedwing_althold_dir = 1;

    // Motor/ESC/Servo
    resetEscAndServoConfig(&masterConfig.escAndServoConfig);
    resetFlight3DConfig(&masterConfig.flight3DConfig);

#ifdef BRUSHED_MOTORS
    masterConfig.motor_pwm_rate = BRUSHED_MOTORS_PWM_RATE;
#else
    masterConfig.motor_pwm_rate = BRUSHLESS_MOTORS_PWM_RATE;
#endif
    masterConfig.servo_pwm_rate = 50;

#ifdef GPS
    // gps/nav stuff
    masterConfig.gpsConfig.autoConfig = GPS_AUTOCONFIG_ON;
#endif

    resetSerialConfig(&masterConfig.serialConfig);

    masterConfig.looptime = 2000;
    masterConfig.i2c_highspeed = 1;
    masterConfig.gyroSync = 1;
    masterConfig.gyroSyncDenominator = 1;

    resetPidProfile(&currentProfile->pidProfile);

    resetControlRateConfig(&masterConfig.controlRateProfiles[0]);

    // for (i = 0; i < CHECKBOXITEMS; i++)
    //     cfg.activate[i] = 0;

    resetRollAndPitchTrims(&currentProfile->accelerometerTrims);

    currentProfile->mag_declination = 0;
    currentProfile->acc_cut_hz = 15;
    currentProfile->accz_lpf_cutoff = 5.0f;
    currentProfile->accDeadband.xy = 40;
    currentProfile->accDeadband.z = 40;
    currentProfile->acc_unarmedcal = 1;

#ifdef BARO
    resetBarometerConfig(&currentProfile->barometerConfig);
#endif

    // Radio
    parseRcChannels("AETR1234", &masterConfig.rxConfig);

    resetRcControlsConfig(&currentProfile->rcControlsConfig);

    currentProfile->throttle_correction_value = 0;      // could 10 with althold or 40 for fpv
    currentProfile->throttle_correction_angle = 800;    // could be 80.0 deg with atlhold or 45.0 for fpv

    // Failsafe Variables
    masterConfig.failsafeConfig.failsafe_delay = 10;              // 1sec
    masterConfig.failsafeConfig.failsafe_off_delay = 200;         // 20sec
    masterConfig.failsafeConfig.failsafe_throttle = 1000;         // default throttle off.
    masterConfig.failsafeConfig.failsafe_throttle_low_delay = 100; // default throttle low delay for "just disarm" on failsafe condition

#ifdef USE_SERVOS
    // servos
    for (i = 0; i < MAX_SUPPORTED_SERVOS; i++) {
        currentProfile->servoConf[i].min = DEFAULT_SERVO_MIN;
        currentProfile->servoConf[i].max = DEFAULT_SERVO_MAX;
        currentProfile->servoConf[i].middle = DEFAULT_SERVO_MIDDLE;
        currentProfile->servoConf[i].rate = 100;
        currentProfile->servoConf[i].angleAtMin = DEFAULT_SERVO_MIN_ANGLE;
        currentProfile->servoConf[i].angleAtMax = DEFAULT_SERVO_MAX_ANGLE;
        currentProfile->servoConf[i].forwardFromChannel = CHANNEL_FORWARDING_DISABLED;
    }

    // gimbal
    currentProfile->gimbalConfig.mode = GIMBAL_MODE_NORMAL;
#endif

#ifdef GPS
    resetGpsProfile(&currentProfile->gpsProfile);
#endif

#ifdef LED_STRIP
    applyDefaultColors(masterConfig.colors, CONFIGURABLE_COLOR_COUNT);
    applyDefaultLedStripConfig(masterConfig.ledConfigs);
#endif

#ifdef TRANSPONDER
    static const uint8_t defaultTransponderData[6] = { 0x12, 0x34, 0x56, 0x78, 0x9A, 0xBC }; // Note, this is NOT a valid transponder code, it's just for testing production hardware

    memcpy(masterConfig.transponderData, &defaultTransponderData, sizeof(defaultTransponderData));
#endif

#ifdef BLACKBOX

#if defined(ENABLE_BLACKBOX_LOGGING_ON_SPIFLASH_BY_DEFAULT)
    featureSet(FEATURE_BLACKBOX);
    masterConfig.blackbox_device = BLACKBOX_DEVICE_FLASH;
#elif defined(ENABLE_BLACKBOX_LOGGING_ON_SDCARD_BY_DEFAULT)
    featureSet(FEATURE_BLACKBOX);
    masterConfig.blackbox_device = BLACKBOX_DEVICE_SDCARD;
#else
    masterConfig.blackbox_device = BLACKBOX_DEVICE_SERIAL;
#endif

    masterConfig.blackbox_rate_num = 1;
    masterConfig.blackbox_rate_denom = 1;
#endif

    // alternative defaults settings for COLIBRI RACE targets
#if defined(COLIBRI_RACE)
    masterConfig.looptime = 1000;

    currentProfile->pidProfile.pidController = 1;

    masterConfig.rxConfig.rcmap[0] = 1;
    masterConfig.rxConfig.rcmap[1] = 2;
    masterConfig.rxConfig.rcmap[2] = 3;
    masterConfig.rxConfig.rcmap[3] = 0;
    masterConfig.rxConfig.rcmap[4] = 4;
    masterConfig.rxConfig.rcmap[5] = 5;
    masterConfig.rxConfig.rcmap[6] = 6;
    masterConfig.rxConfig.rcmap[7] = 7;

    featureSet(FEATURE_ONESHOT125);
    featureSet(FEATURE_VBAT);
    featureSet(FEATURE_LED_STRIP);
    featureSet(FEATURE_FAILSAFE);
#endif

    // alternative defaults settings for ALIENWIIF1 and ALIENWIIF3 targets
#ifdef ALIENWII32
    featureSet(FEATURE_RX_SERIAL);
    featureSet(FEATURE_MOTOR_STOP);
#ifdef ALIENWIIF3
    masterConfig.serialConfig.portConfigs[2].functionMask = FUNCTION_RX_SERIAL;
    masterConfig.batteryConfig.vbatscale = 20;
#else
    masterConfig.serialConfig.portConfigs[1].functionMask = FUNCTION_RX_SERIAL;
#endif
    masterConfig.rxConfig.serialrx_provider = 1;
    masterConfig.rxConfig.spektrum_sat_bind = 5;
    masterConfig.escAndServoConfig.minthrottle = 1000;
    masterConfig.escAndServoConfig.maxthrottle = 2000;
    masterConfig.motor_pwm_rate = 32000;
    masterConfig.looptime = 2000;
    currentProfile->pidProfile.pidController = 3;
    currentProfile->pidProfile.P8[ROLL] = 36;
    currentProfile->pidProfile.P8[PITCH] = 36;
    masterConfig.failsafeConfig.failsafe_delay = 2;
    masterConfig.failsafeConfig.failsafe_off_delay = 0;
    currentControlRateProfile->rcRate8 = 130;
    currentControlRateProfile->rates[FD_PITCH] = 20;
    currentControlRateProfile->rates[FD_ROLL] = 20;
    currentControlRateProfile->rates[FD_YAW] = 100;
    parseRcChannels("TAER1234", &masterConfig.rxConfig);

    //  { 1.0f, -0.414178f,  1.0f, -1.0f },          // REAR_R
    masterConfig.customMotorMixer[0].throttle = 1.0f;
    masterConfig.customMotorMixer[0].roll = -0.414178f;
    masterConfig.customMotorMixer[0].pitch = 1.0f;
    masterConfig.customMotorMixer[0].yaw = -1.0f;

    //  { 1.0f, -0.414178f, -1.0f,  1.0f },          // FRONT_R
    masterConfig.customMotorMixer[1].throttle = 1.0f;
    masterConfig.customMotorMixer[1].roll = -0.414178f;
    masterConfig.customMotorMixer[1].pitch = -1.0f;
    masterConfig.customMotorMixer[1].yaw = 1.0f;

    //  { 1.0f,  0.414178f,  1.0f,  1.0f },          // REAR_L
    masterConfig.customMotorMixer[2].throttle = 1.0f;
    masterConfig.customMotorMixer[2].roll = 0.414178f;
    masterConfig.customMotorMixer[2].pitch = 1.0f;
    masterConfig.customMotorMixer[2].yaw = 1.0f;

    //  { 1.0f,  0.414178f, -1.0f, -1.0f },          // FRONT_L
    masterConfig.customMotorMixer[3].throttle = 1.0f;
    masterConfig.customMotorMixer[3].roll = 0.414178f;
    masterConfig.customMotorMixer[3].pitch = -1.0f;
    masterConfig.customMotorMixer[3].yaw = -1.0f;

    //  { 1.0f, -1.0f, -0.414178f, -1.0f },          // MIDFRONT_R
    masterConfig.customMotorMixer[4].throttle = 1.0f;
    masterConfig.customMotorMixer[4].roll = -1.0f;
    masterConfig.customMotorMixer[4].pitch = -0.414178f;
    masterConfig.customMotorMixer[4].yaw = -1.0f;

    //  { 1.0f,  1.0f, -0.414178f,  1.0f },          // MIDFRONT_L
    masterConfig.customMotorMixer[5].throttle = 1.0f;
    masterConfig.customMotorMixer[5].roll = 1.0f;
    masterConfig.customMotorMixer[5].pitch = -0.414178f;
    masterConfig.customMotorMixer[5].yaw = 1.0f;

    //  { 1.0f, -1.0f,  0.414178f,  1.0f },          // MIDREAR_R
    masterConfig.customMotorMixer[6].throttle = 1.0f;
    masterConfig.customMotorMixer[6].roll = -1.0f;
    masterConfig.customMotorMixer[6].pitch = 0.414178f;
    masterConfig.customMotorMixer[6].yaw = 1.0f;

    //  { 1.0f,  1.0f,  0.414178f, -1.0f },          // MIDREAR_L
    masterConfig.customMotorMixer[7].throttle = 1.0f;
    masterConfig.customMotorMixer[7].roll = 1.0f;
    masterConfig.customMotorMixer[7].pitch = 0.414178f;
    masterConfig.customMotorMixer[7].yaw = -1.0f;
#endif

    // copy first profile into remaining profile
    for (i = 1; i < MAX_PROFILE_COUNT; i++) {
        memcpy(&masterConfig.profile[i], currentProfile, sizeof(profile_t));
    }

    // copy first control rate config into remaining profile
    for (i = 1; i < MAX_CONTROL_RATE_PROFILE_COUNT; i++) {
        memcpy(&masterConfig.controlRateProfiles[i], currentControlRateProfile, sizeof(controlRateConfig_t));
    }

    for (i = 1; i < MAX_PROFILE_COUNT; i++) {
        masterConfig.profile[i].defaultRateProfileIndex = i % MAX_CONTROL_RATE_PROFILE_COUNT;
    }
}