Esempio n. 1
0
//********************************************************************************
//This function does all the calibrations, etc. that we need during a ground start
//********************************************************************************
void Rover::startup_ground(void)
{
    set_mode(INITIALISING);
    
	gcs_send_text(MAV_SEVERITY_INFO,"<startup_ground> Ground start");

	#if(GROUND_START_DELAY > 0)
		gcs_send_text(MAV_SEVERITY_NOTICE,"<startup_ground> With delay");
		delay(GROUND_START_DELAY * 1000);
	#endif

	//IMU ground start
	//------------------------
    //

	startup_INS_ground();

	// read the radio to set trims
	// ---------------------------
	trim_radio();

    // initialise mission library
    mission.init();

    // we don't want writes to the serial port to cause us to pause
    // so set serial ports non-blocking once we are ready to drive
    serial_manager.set_blocking_writes_all(false);

    ins.set_raw_logging(should_log(MASK_LOG_IMU_RAW));
    ins.set_dataflash(&DataFlash);

	gcs_send_text(MAV_SEVERITY_INFO,"Ready to drive");
}
Esempio n. 2
0
//********************************************************************************
//This function does all the calibrations, etc. that we need during a ground start
//********************************************************************************
void Plane::startup_ground(void)
{
    set_mode(INITIALISING);

    gcs_send_text_P(SEVERITY_LOW,PSTR("<startup_ground> GROUND START"));

#if (GROUND_START_DELAY > 0)
    gcs_send_text_P(SEVERITY_LOW,PSTR("<startup_ground> With Delay"));
    delay(GROUND_START_DELAY * 1000);
#endif

    // Makes the servos wiggle
    // step 1 = 1 wiggle
    // -----------------------
    if (!g.skip_gyro_cal) {
        demo_servos(1);
    }

    //INS ground start
    //------------------------
    //
    startup_INS_ground();

    // read the radio to set trims
    // ---------------------------
    if (g.trim_rc_at_start != 0) {
        trim_radio();
    }

    // Save the settings for in-air restart
    // ------------------------------------
    //save_EEPROM_groundstart();

    // initialise mission library
    mission.init();

    // Makes the servos wiggle - 3 times signals ready to fly
    // -----------------------
    if (!g.skip_gyro_cal) {
        demo_servos(3);
    }

    // reset last heartbeat time, so we don't trigger failsafe on slow
    // startup
    failsafe.last_heartbeat_ms = millis();

    // we don't want writes to the serial port to cause us to pause
    // mid-flight, so set the serial ports non-blocking once we are
    // ready to fly
    serial_manager.set_blocking_writes_all(false);

    ins.set_raw_logging(should_log(MASK_LOG_IMU_RAW));
    ins.set_dataflash(&DataFlash);    

    gcs_send_text_P(SEVERITY_LOW,PSTR("\n\n Ready to FLY."));
}
Esempio n. 3
0
//********************************************************************************
//This function does all the calibrations, etc. that we need during a ground start
//********************************************************************************
void Plane::startup_ground(void)
{
    set_mode(INITIALISING, MODE_REASON_UNKNOWN);

    gcs_send_text(MAV_SEVERITY_INFO,"<startup_ground> Ground start");

#if (GROUND_START_DELAY > 0)
    gcs_send_text(MAV_SEVERITY_NOTICE,"<startup_ground> With delay");
    delay(GROUND_START_DELAY * 1000);
#endif

    //INS ground start
    //------------------------
    //
    startup_INS_ground();

    // read the radio to set trims
    // ---------------------------
    if (g.trim_rc_at_start != 0) {
        trim_radio();
    }

    // Save the settings for in-air restart
    // ------------------------------------
    //save_EEPROM_groundstart();

    // initialise mission library
    mission.init();

    // reset last heartbeat time, so we don't trigger failsafe on slow
    // startup
    failsafe.last_heartbeat_ms = millis();

    // we don't want writes to the serial port to cause us to pause
    // mid-flight, so set the serial ports non-blocking once we are
    // ready to fly
    serial_manager.set_blocking_writes_all(false);

    ins.set_raw_logging(should_log(MASK_LOG_IMU_RAW));
    ins.set_dataflash(&DataFlash);

    gcs_send_text(MAV_SEVERITY_INFO,"Ready to fly");
}
Esempio n. 4
0
void Copter::init_ardupilot()
{
    if (!hal.gpio->usb_connected()) {
        // USB is not connected, this means UART0 may be a Xbee, with
        // its darned bricking problem. We can't write to it for at
        // least one second after powering up. Simplest solution for
        // now is to delay for 1 second. Something more elegant may be
        // added later
        delay(1000);
    }

    // initialise serial port
    serial_manager.init_console();

    // init vehicle capabilties
    init_capabilities();

    cliSerial->printf("\n\nInit " FIRMWARE_STRING
                         "\n\nFree RAM: %u\n",
                      (unsigned)hal.util->available_memory());

    //
    // Report firmware version code expect on console (check of actual EEPROM format version is done in load_parameters function)
    //
    report_version();

    // load parameters from EEPROM
    load_parameters();

    BoardConfig.init();

    // initialise serial port
    serial_manager.init();

    // init EPM cargo gripper
#if EPM_ENABLED == ENABLED
    epm.init();
#endif

    // initialise notify system
    // disable external leds if epm is enabled because of pin conflict on the APM
    notify.init(true);

    // initialise battery monitor
    battery.init();

    // Init RSSI
    rssi.init();
    
    barometer.init();

    // Register the mavlink service callback. This will run
    // anytime there are more than 5ms remaining in a call to
    // hal.scheduler->delay.
    hal.scheduler->register_delay_callback(mavlink_delay_cb_static, 5);

    // we start by assuming USB connected, as we initialed the serial
    // port with SERIAL0_BAUD. check_usb_mux() fixes this if need be.
    ap.usb_connected = true;
    check_usb_mux();

    // init the GCS connected to the console
    gcs[0].setup_uart(serial_manager, AP_SerialManager::SerialProtocol_Console, 0);

    // init telemetry port
    gcs[1].setup_uart(serial_manager, AP_SerialManager::SerialProtocol_MAVLink, 0);

    // setup serial port for telem2
    gcs[2].setup_uart(serial_manager, AP_SerialManager::SerialProtocol_MAVLink, 1);

    // setup serial port for fourth telemetry port (not used by default)
    gcs[3].setup_uart(serial_manager, AP_SerialManager::SerialProtocol_MAVLink, 2);

#if FRSKY_TELEM_ENABLED == ENABLED
    // setup frsky
    frsky_telemetry.init(serial_manager);
#endif

    // identify ourselves correctly with the ground station
    mavlink_system.sysid = g.sysid_this_mav;

#if LOGGING_ENABLED == ENABLED
    log_init();
#endif

    GCS_MAVLINK::set_dataflash(&DataFlash);

    // update motor interlock state
    update_using_interlock();

#if FRAME_CONFIG == HELI_FRAME
    // trad heli specific initialisation
    heli_init();
#endif
    
    init_rc_in();               // sets up rc channels from radio
    init_rc_out();              // sets up motors and output to escs

    // initialise which outputs Servo and Relay events can use
    ServoRelayEvents.set_channel_mask(~motors.get_motor_mask());

    relay.init();

    /*
     *  setup the 'main loop is dead' check. Note that this relies on
     *  the RC library being initialised.
     */
    hal.scheduler->register_timer_failsafe(failsafe_check_static, 1000);

    // Do GPS init
    gps.init(&DataFlash, serial_manager);

    if(g.compass_enabled)
        init_compass();

#if OPTFLOW == ENABLED
    // make optflow available to AHRS
    ahrs.set_optflow(&optflow);
#endif

    // init Location class
    Location_Class::set_ahrs(&ahrs);
#if AP_TERRAIN_AVAILABLE && AC_TERRAIN
    Location_Class::set_terrain(&terrain);
    wp_nav.set_terrain(&terrain);
#endif

    pos_control.set_dt(MAIN_LOOP_SECONDS);

    // init the optical flow sensor
    init_optflow();

#if MOUNT == ENABLED
    // initialise camera mount
    camera_mount.init(&DataFlash, serial_manager);
#endif

#if PRECISION_LANDING == ENABLED
    // initialise precision landing
    init_precland();
#endif

#ifdef USERHOOK_INIT
    USERHOOK_INIT
#endif

#if CLI_ENABLED == ENABLED
    if (g.cli_enabled) {
        const char *msg = "\nPress ENTER 3 times to start interactive setup\n";
        cliSerial->println(msg);
        if (gcs[1].initialised && (gcs[1].get_uart() != NULL)) {
            gcs[1].get_uart()->println(msg);
        }
        if (num_gcs > 2 && gcs[2].initialised && (gcs[2].get_uart() != NULL)) {
            gcs[2].get_uart()->println(msg);
        }
    }
#endif // CLI_ENABLED

#if HIL_MODE != HIL_MODE_DISABLED
    while (barometer.get_last_update() == 0) {
        // the barometer begins updating when we get the first
        // HIL_STATE message
        gcs_send_text(MAV_SEVERITY_WARNING, "Waiting for first HIL_STATE message");
        delay(1000);
    }

    // set INS to HIL mode
    ins.set_hil_mode();
#endif

    // read Baro pressure at ground
    //-----------------------------
    init_barometer(true);

    // initialise sonar
#if CONFIG_SONAR == ENABLED
    init_sonar();
#endif

    // initialise AP_RPM library
    rpm_sensor.init();

    // initialise mission library
    mission.init();

    // initialise the flight mode and aux switch
    // ---------------------------
    reset_control_switch();
    init_aux_switches();

    startup_INS_ground();

    // set landed flags
    set_land_complete(true);
    set_land_complete_maybe(true);

    // we don't want writes to the serial port to cause us to pause
    // mid-flight, so set the serial ports non-blocking once we are
    // ready to fly
    serial_manager.set_blocking_writes_all(false);

    // enable CPU failsafe
    failsafe_enable();

    ins.set_raw_logging(should_log(MASK_LOG_IMU_RAW));
    ins.set_dataflash(&DataFlash);

    cliSerial->print("\nReady to FLY ");

    // flag that initialisation has completed
    ap.initialised = true;
}
Esempio n. 5
0
void Sub::init_ardupilot()
{
    if (!hal.gpio->usb_connected()) {
        // USB is not connected, this means UART0 may be a Xbee, with
        // its darned bricking problem. We can't write to it for at
        // least one second after powering up. Simplest solution for
        // now is to delay for 1 second. Something more elegant may be
        // added later
        hal.scheduler->delay(1000);
    }

    // initialise serial port
    serial_manager.init_console();

    cliSerial->printf("\n\nInit " FIRMWARE_STRING
                      "\n\nFree RAM: %u\n",
                      (unsigned)hal.util->available_memory());

    //
    // Report firmware version code expect on console (check of actual EEPROM format version is done in load_parameters function)
    //
    report_version();

    // load parameters from EEPROM
    load_parameters();

    BoardConfig.init();

    // initialise serial port
    serial_manager.init();

    // init cargo gripper
#if GRIPPER_ENABLED == ENABLED
    g2.gripper.init();
#endif

    // initialise notify system
    notify.init(true);

    // initialise battery monitor
    battery.init();

    barometer.init();

    celsius.init();

    // Register the mavlink service callback. This will run
    // anytime there are more than 5ms remaining in a call to
    // hal.scheduler->delay.
    hal.scheduler->register_delay_callback(mavlink_delay_cb_static, 5);

    // we start by assuming USB connected, as we initialed the serial
    // port with SERIAL0_BAUD. check_usb_mux() fixes this if need be.
    ap.usb_connected = true;
    check_usb_mux();

    // setup telem slots with serial ports
    for (uint8_t i = 0; i < MAVLINK_COMM_NUM_BUFFERS; i++) {
        gcs_chan[i].setup_uart(serial_manager, AP_SerialManager::SerialProtocol_MAVLink, i);
    }

    // identify ourselves correctly with the ground station
    mavlink_system.sysid = g.sysid_this_mav;

#if LOGGING_ENABLED == ENABLED
    log_init();
#endif

    gcs().set_dataflash(&DataFlash);

    init_rc_in();               // sets up rc channels from radio
    init_rc_out();              // sets up motors and output to escs
    init_joystick();            // joystick initialization

    // initialise which outputs Servo and Relay events can use
    ServoRelayEvents.set_channel_mask(~motors.get_motor_mask());

    relay.init();

    /*
     *  setup the 'main loop is dead' check. Note that this relies on
     *  the RC library being initialised.
     */
    hal.scheduler->register_timer_failsafe(failsafe_check_static, 1000);

    // Do GPS init
    gps.init(&DataFlash, serial_manager);

    if (g.compass_enabled) {
        init_compass();
    }

#if OPTFLOW == ENABLED
    // make optflow available to AHRS
    ahrs.set_optflow(&optflow);
#endif

    // init Location class
    Location_Class::set_ahrs(&ahrs);
#if AP_TERRAIN_AVAILABLE && AC_TERRAIN
    Location_Class::set_terrain(&terrain);
    wp_nav.set_terrain(&terrain);
#endif

#if AVOIDANCE_ENABLED == ENABLED
    wp_nav.set_avoidance(&avoid);
#endif

    pos_control.set_dt(MAIN_LOOP_SECONDS);

    // init the optical flow sensor
    init_optflow();

#if MOUNT == ENABLED
    // initialise camera mount
    camera_mount.init(&DataFlash, serial_manager);
#endif

#ifdef USERHOOK_INIT
    USERHOOK_INIT
#endif

#if CLI_ENABLED == ENABLED
    if (g.cli_enabled) {
        const char *msg = "\nPress ENTER 3 times to start interactive setup\n";
        cliSerial->println(msg);
        if (gcs_chan[1].initialised && (gcs_chan[1].get_uart() != NULL)) {
            gcs_chan[1].get_uart()->println(msg);
        }
        if (num_gcs > 2 && gcs_chan[2].initialised && (gcs_chan[2].get_uart() != NULL)) {
            gcs_chan[2].get_uart()->println(msg);
        }
    }
#endif // CLI_ENABLED

#if HIL_MODE != HIL_MODE_DISABLED
    while (barometer.get_last_update() == 0) {
        // the barometer begins updating when we get the first
        // HIL_STATE message
        gcs_send_text(MAV_SEVERITY_WARNING, "Waiting for first HIL_STATE message");
        hal.scheduler->delay(1000);
    }

    // set INS to HIL mode
    ins.set_hil_mode();
#endif

    // read Baro pressure at ground
    //-----------------------------
    init_barometer(false);
    barometer.update();

    for (uint8_t i = 0; i < barometer.num_instances(); i++) {
        if (barometer.get_type(i) == AP_Baro::BARO_TYPE_WATER && barometer.healthy(i)) {
            barometer.set_primary_baro(i);
            ap.depth_sensor_present = true;
            break;
        }
    }

    if (!ap.depth_sensor_present) {
        // We only have onboard baro
        // No external underwater depth sensor detected
        barometer.set_primary_baro(0);
        EKF2.set_baro_alt_noise(10.0f); // Readings won't correspond with rest of INS
        EKF3.set_baro_alt_noise(10.0f);
    } else {
        EKF2.set_baro_alt_noise(0.1f);
        EKF3.set_baro_alt_noise(0.1f);
    }

    leak_detector.init();

    // backwards compatibility
    if (attitude_control.get_accel_yaw_max() < 110000.0f) {
        attitude_control.save_accel_yaw_max(110000.0f);
    }

    last_pilot_heading = ahrs.yaw_sensor;

    // initialise rangefinder
#if RANGEFINDER_ENABLED == ENABLED
    init_rangefinder();
#endif

    // initialise AP_RPM library
#if RPM_ENABLED == ENABLED
    rpm_sensor.init();
#endif

    // initialise mission library
    mission.init();

    startup_INS_ground();

    // we don't want writes to the serial port to cause us to pause
    // mid-flight, so set the serial ports non-blocking once we are
    // ready to fly
    serial_manager.set_blocking_writes_all(false);

    // enable CPU failsafe
    failsafe_enable();

    ins.set_raw_logging(should_log(MASK_LOG_IMU_RAW));
    ins.set_dataflash(&DataFlash);

    // init vehicle capabilties
    init_capabilities();

    cliSerial->print("\nReady to FLY ");

    // flag that initialisation has completed
    ap.initialised = true;
}