// Print the current configuration.
// Called by the setup menu 'show' command.
int8_t Copter::setup_show(uint8_t argc, const Menu::arg *argv)
{
AP_Param *param;
ap_var_type type;
//If a parameter name is given as an argument to show, print only that parameter
if(argc>=2)
{
param=AP_Param::find(argv[1].str, &type);
if(!param)
{
cliSerial->printf("Parameter not found: '%s'\n", argv[1].str);
return 0;
}
AP_Param::show(param, argv[1].str, type, cliSerial);
return 0;
}
// clear the area
print_blanks(8);
report_version();
report_radio();
report_frame();
report_batt_monitor();
report_flight_modes();
report_ins();
report_compass();
report_optflow();
AP_Param::show_all(cliSerial);
return(0);
}
// setup_compassmot - sets compass's motor interference parameters
uint8_t Copter::mavlink_compassmot(mavlink_channel_t chan)
{
#if FRAME_CONFIG == HELI_FRAME
// compassmot not implemented for tradheli
return 1;
#else
int8_t comp_type; // throttle or current based compensation
Vector3f compass_base[COMPASS_MAX_INSTANCES]; // compass vector when throttle is zero
Vector3f motor_impact[COMPASS_MAX_INSTANCES]; // impact of motors on compass vector
Vector3f motor_impact_scaled[COMPASS_MAX_INSTANCES]; // impact of motors on compass vector scaled with throttle
Vector3f motor_compensation[COMPASS_MAX_INSTANCES]; // final compensation to be stored to eeprom
float throttle_pct; // throttle as a percentage 0.0 ~ 1.0
float throttle_pct_max = 0.0f; // maximum throttle reached (as a percentage 0~1.0)
float current_amps_max = 0.0f; // maximum current reached
float interference_pct[COMPASS_MAX_INSTANCES]; // interference as a percentage of total mag field (for reporting purposes only)
uint32_t last_run_time;
uint32_t last_send_time;
bool updated = false; // have we updated the compensation vector at least once
uint8_t command_ack_start = command_ack_counter;
// exit immediately if we are already in compassmot
if (ap.compass_mot) {
// ignore restart messages
return 1;
}else{
ap.compass_mot = true;
}
// initialise output
for (uint8_t i=0; i<COMPASS_MAX_INSTANCES; i++) {
interference_pct[i] = 0.0f;
}
// check compass is enabled
if (!g.compass_enabled) {
gcs[chan-MAVLINK_COMM_0].send_text(MAV_SEVERITY_CRITICAL, "Compass disabled");
ap.compass_mot = false;
return 1;
}
// check compass health
compass.read();
for (uint8_t i=0; i<compass.get_count(); i++) {
if (!compass.healthy(i)) {
gcs[chan-MAVLINK_COMM_0].send_text(MAV_SEVERITY_CRITICAL, "Check compass");
ap.compass_mot = false;
return 1;
}
}
// check if radio is calibrated
pre_arm_rc_checks();
if (!ap.pre_arm_rc_check) {
gcs[chan-MAVLINK_COMM_0].send_text(MAV_SEVERITY_CRITICAL, "RC not calibrated");
ap.compass_mot = false;
return 1;
}
// check throttle is at zero
read_radio();
if (channel_throttle->control_in != 0) {
gcs[chan-MAVLINK_COMM_0].send_text(MAV_SEVERITY_CRITICAL, "Throttle not zero");
ap.compass_mot = false;
return 1;
}
// check we are landed
if (!ap.land_complete) {
gcs[chan-MAVLINK_COMM_0].send_text(MAV_SEVERITY_CRITICAL, "Not landed");
ap.compass_mot = false;
return 1;
}
// disable cpu failsafe
failsafe_disable();
// initialise compass
init_compass();
// default compensation type to use current if possible
if (battery.has_current()) {
comp_type = AP_COMPASS_MOT_COMP_CURRENT;
}else{
comp_type = AP_COMPASS_MOT_COMP_THROTTLE;
}
// send back initial ACK
mavlink_msg_command_ack_send(chan, MAV_CMD_PREFLIGHT_CALIBRATION,0);
// flash leds
AP_Notify::flags.esc_calibration = true;
// warn user we are starting calibration
gcs[chan-MAVLINK_COMM_0].send_text(MAV_SEVERITY_INFO, "Starting calibration");
// inform what type of compensation we are attempting
if (comp_type == AP_COMPASS_MOT_COMP_CURRENT) {
gcs[chan-MAVLINK_COMM_0].send_text(MAV_SEVERITY_INFO, "Current");
} else{
gcs[chan-MAVLINK_COMM_0].send_text(MAV_SEVERITY_INFO, "Throttle");
}
// disable throttle and battery failsafe
g.failsafe_throttle = FS_THR_DISABLED;
g.failsafe_battery_enabled = FS_BATT_DISABLED;
// disable motor compensation
compass.motor_compensation_type(AP_COMPASS_MOT_COMP_DISABLED);
for (uint8_t i=0; i<compass.get_count(); i++) {
compass.set_motor_compensation(i, Vector3f(0,0,0));
}
// get initial compass readings
last_run_time = millis();
while ( millis() - last_run_time < 500 ) {
compass.accumulate();
}
compass.read();
// store initial x,y,z compass values
// initialise interference percentage
for (uint8_t i=0; i<compass.get_count(); i++) {
compass_base[i] = compass.get_field(i);
interference_pct[i] = 0.0f;
}
// enable motors and pass through throttle
init_rc_out();
enable_motor_output();
motors.armed(true);
// initialise run time
last_run_time = millis();
last_send_time = millis();
// main run while there is no user input and the compass is healthy
while (command_ack_start == command_ack_counter && compass.healthy(compass.get_primary()) && motors.armed()) {
// 50hz loop
if (millis() - last_run_time < 20) {
// grab some compass values
compass.accumulate();
hal.scheduler->delay(5);
continue;
}
last_run_time = millis();
// read radio input
read_radio();
// pass through throttle to motors
motors.throttle_pass_through(channel_throttle->radio_in);
// read some compass values
compass.read();
// read current
read_battery();
// calculate scaling for throttle
throttle_pct = (float)channel_throttle->control_in / 1000.0f;
throttle_pct = constrain_float(throttle_pct,0.0f,1.0f);
// if throttle is near zero, update base x,y,z values
if (throttle_pct <= 0.0f) {
for (uint8_t i=0; i<compass.get_count(); i++) {
compass_base[i] = compass_base[i] * 0.99f + compass.get_field(i) * 0.01f;
}
// causing printing to happen as soon as throttle is lifted
} else {
// calculate diff from compass base and scale with throttle
for (uint8_t i=0; i<compass.get_count(); i++) {
motor_impact[i] = compass.get_field(i) - compass_base[i];
}
// throttle based compensation
if (comp_type == AP_COMPASS_MOT_COMP_THROTTLE) {
// for each compass
for (uint8_t i=0; i<compass.get_count(); i++) {
// scale by throttle
motor_impact_scaled[i] = motor_impact[i] / throttle_pct;
// adjust the motor compensation to negate the impact
motor_compensation[i] = motor_compensation[i] * 0.99f - motor_impact_scaled[i] * 0.01f;
}
updated = true;
} else {
// for each compass
for (uint8_t i=0; i<compass.get_count(); i++) {
// current based compensation if more than 3amps being drawn
motor_impact_scaled[i] = motor_impact[i] / battery.current_amps();
// adjust the motor compensation to negate the impact if drawing over 3amps
if (battery.current_amps() >= 3.0f) {
motor_compensation[i] = motor_compensation[i] * 0.99f - motor_impact_scaled[i] * 0.01f;
updated = true;
}
}
}
// calculate interference percentage at full throttle as % of total mag field
if (comp_type == AP_COMPASS_MOT_COMP_THROTTLE) {
for (uint8_t i=0; i<compass.get_count(); i++) {
// interference is impact@fullthrottle / mag field * 100
interference_pct[i] = motor_compensation[i].length() / (float)COMPASS_MAGFIELD_EXPECTED * 100.0f;
}
}else{
for (uint8_t i=0; i<compass.get_count(); i++) {
// interference is impact/amp * (max current seen / max throttle seen) / mag field * 100
interference_pct[i] = motor_compensation[i].length() * (current_amps_max/throttle_pct_max) / (float)COMPASS_MAGFIELD_EXPECTED * 100.0f;
}
}
// record maximum throttle and current
throttle_pct_max = MAX(throttle_pct_max, throttle_pct);
current_amps_max = MAX(current_amps_max, battery.current_amps());
}
if (AP_HAL::millis() - last_send_time > 500) {
last_send_time = AP_HAL::millis();
mavlink_msg_compassmot_status_send(chan,
channel_throttle->control_in,
battery.current_amps(),
interference_pct[compass.get_primary()],
motor_compensation[compass.get_primary()].x,
motor_compensation[compass.get_primary()].y,
motor_compensation[compass.get_primary()].z);
}
}
// stop motors
motors.output_min();
motors.armed(false);
// set and save motor compensation
if (updated) {
compass.motor_compensation_type(comp_type);
for (uint8_t i=0; i<compass.get_count(); i++) {
compass.set_motor_compensation(i, motor_compensation[i]);
}
compass.save_motor_compensation();
// display success message
gcs[chan-MAVLINK_COMM_0].send_text(MAV_SEVERITY_INFO, "Calibration successful");
} else {
// compensation vector never updated, report failure
gcs[chan-MAVLINK_COMM_0].send_text(MAV_SEVERITY_NOTICE, "Failed");
compass.motor_compensation_type(AP_COMPASS_MOT_COMP_DISABLED);
}
// display new motor offsets and save
report_compass();
// turn off notify leds
AP_Notify::flags.esc_calibration = false;
// re-enable cpu failsafe
failsafe_enable();
// re-enable failsafes
g.failsafe_throttle.load();
g.failsafe_battery_enabled.load();
// flag we have completed
ap.compass_mot = false;
return 0;
#endif // FRAME_CONFIG != HELI_FRAME
}
int8_t Sub::test_compass(uint8_t argc, const Menu::arg *argv)
{
uint8_t delta_ms_fast_loop;
uint8_t medium_loopCounter = 0;
if (!g.compass_enabled) {
cliSerial->printf("Compass: "******"Compass initialisation failed!");
return 0;
}
ahrs.init();
ahrs.set_fly_forward(true);
ahrs.set_compass(&compass);
#if OPTFLOW == ENABLED
ahrs.set_optflow(&optflow);
#endif
report_compass();
// we need the AHRS initialised for this test
ins.init(scheduler.get_loop_rate_hz());
ahrs.reset();
int16_t counter = 0;
float heading = 0;
print_hit_enter();
while(1) {
delay(20);
if (millis() - fast_loopTimer > 19) {
delta_ms_fast_loop = millis() - fast_loopTimer;
G_Dt = (float)delta_ms_fast_loop / 1000.0f; // used by DCM integrator
fast_loopTimer = millis();
// INS
// ---
ahrs.update();
medium_loopCounter++;
if(medium_loopCounter == 5) {
if (compass.read()) {
// Calculate heading
const Matrix3f &m = ahrs.get_rotation_body_to_ned();
heading = compass.calculate_heading(m);
compass.learn_offsets();
}
medium_loopCounter = 0;
}
counter++;
if (counter>20) {
if (compass.healthy()) {
const Vector3f &mag_ofs = compass.get_offsets();
const Vector3f &mag = compass.get_field();
cliSerial->printf("Heading: %d, XYZ: %.0f, %.0f, %.0f,\tXYZoff: %6.2f, %6.2f, %6.2f\n",
(int)(wrap_360_cd(ToDeg(heading) * 100)) /100,
(double)mag.x,
(double)mag.y,
(double)mag.z,
(double)mag_ofs.x,
(double)mag_ofs.y,
(double)mag_ofs.z);
} else {
cliSerial->println("compass not healthy");
}
counter=0;
}
}
if (cliSerial->available() > 0) {
break;
}
}
// save offsets. This allows you to get sane offset values using
// the CLI before you go flying.
cliSerial->println("saving offsets");
compass.save_offsets();
return (0);
}