int8_t Plane::test_failsafe(uint8_t argc, const Menu::arg *argv)
{
uint8_t fail_test;
print_hit_enter();
for(int16_t i = 0; i < 50; i++) {
hal.scheduler->delay(20);
read_radio();
}
// read the radio to set trims
// ---------------------------
trim_radio();
oldSwitchPosition = readSwitch();
cliSerial->printf_P(PSTR("Unplug battery, throttle in neutral, turn off radio.\n"));
while(channel_throttle->control_in > 0) {
hal.scheduler->delay(20);
read_radio();
}
while(1) {
hal.scheduler->delay(20);
read_radio();
if(channel_throttle->control_in > 0) {
cliSerial->printf_P(PSTR("THROTTLE CHANGED %d \n"), (int)channel_throttle->control_in);
fail_test++;
}
if(oldSwitchPosition != readSwitch()) {
cliSerial->printf_P(PSTR("CONTROL MODE CHANGED: "));
print_flight_mode(cliSerial, readSwitch());
cliSerial->println();
fail_test++;
}
if(rc_failsafe_active()) {
cliSerial->printf_P(PSTR("THROTTLE FAILSAFE ACTIVATED: %d, "), (int)channel_throttle->radio_in);
print_flight_mode(cliSerial, readSwitch());
cliSerial->println();
fail_test++;
}
if(fail_test > 0) {
return (0);
}
if(cliSerial->available() > 0) {
cliSerial->printf_P(PSTR("LOS caused no change in APM.\n"));
return (0);
}
}
}
int8_t Rover::test_failsafe(uint8_t argc, const Menu::arg *argv)
{
uint8_t fail_test = 0;
print_hit_enter();
for(int i = 0; i < 50; i++){
delay(20);
read_radio();
}
// read the radio to set trims
// ---------------------------
trim_radio();
oldSwitchPosition = readSwitch();
cliSerial->println("Unplug battery, throttle in neutral, turn off radio.");
while(channel_throttle->get_control_in() > 0){
delay(20);
read_radio();
}
while(1){
delay(20);
read_radio();
if(channel_throttle->get_control_in() > 0){
cliSerial->printf("THROTTLE CHANGED %d \n", channel_throttle->get_control_in());
fail_test++;
}
if (oldSwitchPosition != readSwitch()){
cliSerial->print("CONTROL MODE CHANGED: ");
print_mode(cliSerial, readSwitch());
cliSerial->println();
fail_test++;
}
if(throttle_failsafe_active()) {
cliSerial->printf("THROTTLE FAILSAFE ACTIVATED: %d, ", channel_throttle->get_radio_in());
print_mode(cliSerial, readSwitch());
cliSerial->println();
fail_test++;
}
if(fail_test > 0){
return (0);
}
if(cliSerial->available() > 0){
cliSerial->println("LOS caused no change in APM.");
return (0);
}
}
}
// rc_loops - reads user input from transmitter/receiver
// called at 100hz
void Copter::rc_loop()
{
// Read radio and 3-position switch on radio
// -----------------------------------------
read_radio();
rc().read_mode_switch();
}
// esc_calibration_passthrough - pass through pilot throttle to escs
void Copter::esc_calibration_passthrough()
{
#if FRAME_CONFIG != HELI_FRAME
// clear esc flag for next time
g.esc_calibrate.set_and_save(ESCCAL_NONE);
// reduce update rate to motors to 50Hz
motors.set_update_rate(50);
// send message to GCS
gcs_send_text_P(MAV_SEVERITY_CRITICAL,PSTR("ESC Calibration: passing pilot throttle to ESCs"));
while(1) {
// arm motors
motors.armed(true);
motors.enable();
// flash LEDS
AP_Notify::flags.esc_calibration = true;
// read pilot input
read_radio();
delay(10);
// pass through to motors
motors.throttle_pass_through(channel_throttle->radio_in);
}
#endif // FRAME_CONFIG != HELI_FRAME
}
void Rover::trim_radio()
{
for (uint8_t y = 0; y < 30; y++) {
read_radio();
}
trim_control_surfaces();
}
int8_t Plane::test_radio_pwm(uint8_t argc, const Menu::arg *argv)
{
print_hit_enter();
hal.scheduler->delay(1000);
while(1) {
hal.scheduler->delay(20);
// Filters radio input - adjust filters in the radio.pde file
// ----------------------------------------------------------
read_radio();
cliSerial->printf_P(PSTR("IN:\t1: %d\t2: %d\t3: %d\t4: %d\t5: %d\t6: %d\t7: %d\t8: %d\n"),
(int)channel_roll->radio_in,
(int)channel_pitch->radio_in,
(int)channel_throttle->radio_in,
(int)channel_rudder->radio_in,
(int)g.rc_5.radio_in,
(int)g.rc_6.radio_in,
(int)g.rc_7.radio_in,
(int)g.rc_8.radio_in);
if(cliSerial->available() > 0) {
return (0);
}
}
}
// rc_loops - reads user input from transmitter/receiver
// called at 100hz
void Sub::rc_loop()
{
// Read radio
// -----------------------------------------
read_radio();
failsafe_manual_control_check();
}
int8_t Rover::test_radio_pwm(uint8_t argc, const Menu::arg *argv)
{
print_hit_enter();
delay(1000);
while(1){
delay(20);
// Filters radio input - adjust filters in the radio.cpp file
// ----------------------------------------------------------
read_radio();
cliSerial->printf("IN:\t1: %d\t2: %d\t3: %d\t4: %d\t5: %d\t6: %d\t7: %d\t8: %d\n",
channel_steer->get_radio_in(),
g.rc_2.get_radio_in(),
channel_throttle->get_radio_in(),
g.rc_4.get_radio_in(),
g.rc_5.get_radio_in(),
g.rc_6.get_radio_in(),
g.rc_7.get_radio_in(),
g.rc_8.get_radio_in());
if(cliSerial->available() > 0){
return (0);
}
}
}
int8_t Rover::test_radio(uint8_t argc, const Menu::arg *argv)
{
print_hit_enter();
delay(1000);
// read the radio to set trims
// ---------------------------
trim_radio();
while(1){
delay(20);
read_radio();
channel_steer->calc_pwm();
channel_throttle->calc_pwm();
// write out the servo PWM values
// ------------------------------
set_servos();
cliSerial->printf("IN 1: %d\t2: %d\t3: %d\t4: %d\t5: %d\t6: %d\t7: %d\t8: %d\n",
channel_steer->get_control_in(),
g.rc_2.get_control_in(),
channel_throttle->get_control_in(),
g.rc_4.get_control_in(),
g.rc_5.get_control_in(),
g.rc_6.get_control_in(),
g.rc_7.get_control_in(),
g.rc_8.get_control_in());
if(cliSerial->available() > 0){
return (0);
}
}
}
// rc_loops - reads user input from transmitter/receiver
// called at 100hz
void Copter::rc_loop()
{
// Read radio and 3-position switch on radio
// -----------------------------------------
read_radio();
read_control_switch();
}
// init_rc_out -- initialise motors and check if pilot wants to perform ESC calibration
void Copter::init_rc_out()
{
motors.set_update_rate(g.rc_speed);
motors.set_frame_orientation(g.frame_orientation);
motors.set_loop_rate(scheduler.get_loop_rate_hz());
motors.Init(); // motor initialisation
#if FRAME_CONFIG != HELI_FRAME
motors.set_throttle_range(channel_throttle->get_radio_min(), channel_throttle->get_radio_max());
#endif
for(uint8_t i = 0; i < 5; i++) {
delay(20);
read_radio();
}
// we want the input to be scaled correctly
channel_throttle->set_range_out(0,1000);
// setup correct scaling for ESCs like the UAVCAN PX4ESC which
// take a proportion of speed.
hal.rcout->set_esc_scaling(channel_throttle->get_radio_min(), channel_throttle->get_radio_max());
// check if we should enter esc calibration mode
esc_calibration_startup_check();
// enable output to motors
pre_arm_rc_checks();
if (ap.pre_arm_rc_check) {
enable_motor_output();
}
// refresh auxiliary channel to function map
RC_Channel_aux::update_aux_servo_function();
}
void Rover::trim_control_surfaces()
{
read_radio();
// Store control surface trim values
// ---------------------------------
if ((channel_steer->get_radio_in() > 1400) && (channel_steer->get_radio_in() < 1600)) {
channel_steer->set_radio_trim(channel_steer->get_radio_in());
// save to eeprom
channel_steer->save_eeprom();
}
}
void Plane::trim_control_surfaces()
{
read_radio();
int16_t trim_roll_range = (channel_roll->radio_max - channel_roll->radio_min)/5;
int16_t trim_pitch_range = (channel_pitch->radio_max - channel_pitch->radio_min)/5;
if (channel_roll->radio_in < channel_roll->radio_min+trim_roll_range ||
channel_roll->radio_in > channel_roll->radio_max-trim_roll_range ||
channel_pitch->radio_in < channel_pitch->radio_min+trim_pitch_range ||
channel_pitch->radio_in > channel_pitch->radio_max-trim_pitch_range) {
// don't trim for extreme values - if we attempt to trim so
// there is less than 20 percent range left then assume the
// sticks are not properly centered. This also prevents
// problems with starting APM with the TX off
return;
}
// Store control surface trim values
// ---------------------------------
if(g.mix_mode == 0) {
if (channel_roll->radio_in != 0) {
channel_roll->radio_trim = channel_roll->radio_in;
}
if (channel_pitch->radio_in != 0) {
channel_pitch->radio_trim = channel_pitch->radio_in;
}
// the secondary aileron/elevator is trimmed only if it has a
// corresponding transmitter input channel, which k_aileron
// doesn't have
RC_Channel_aux::set_radio_trim(RC_Channel_aux::k_aileron_with_input);
RC_Channel_aux::set_radio_trim(RC_Channel_aux::k_elevator_with_input);
} else{
if (elevon.ch1_temp != 0) {
elevon.trim1 = elevon.ch1_temp;
}
if (elevon.ch2_temp != 0) {
elevon.trim2 = elevon.ch2_temp;
}
//Recompute values here using new values for elevon1_trim and elevon2_trim
//We cannot use radio_in[CH_ROLL] and radio_in[CH_PITCH] values from read_radio() because the elevon trim values have changed
uint16_t center = 1500;
channel_roll->radio_trim = center;
channel_pitch->radio_trim = center;
}
if (channel_rudder->radio_in != 0) {
channel_rudder->radio_trim = channel_rudder->radio_in;
}
// save to eeprom
channel_roll->save_eeprom();
channel_pitch->save_eeprom();
channel_rudder->save_eeprom();
}
void Plane::trim_control_surfaces()
{
read_radio();
int16_t trim_roll_range = (channel_roll->get_radio_max() - channel_roll->get_radio_min())/5;
int16_t trim_pitch_range = (channel_pitch->get_radio_max() - channel_pitch->get_radio_min())/5;
if (channel_roll->get_radio_in() < channel_roll->get_radio_min()+trim_roll_range ||
channel_roll->get_radio_in() > channel_roll->get_radio_max()-trim_roll_range ||
channel_pitch->get_radio_in() < channel_pitch->get_radio_min()+trim_pitch_range ||
channel_pitch->get_radio_in() > channel_pitch->get_radio_max()-trim_pitch_range) {
// don't trim for extreme values - if we attempt to trim so
// there is less than 20 percent range left then assume the
// sticks are not properly centered. This also prevents
// problems with starting APM with the TX off
return;
}
// trim main surfaces
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_aileron);
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_elevator);
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_rudder);
// trim elevons
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_elevon_left);
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_elevon_right);
// trim vtail
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_vtail_left);
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_vtail_right);
if (SRV_Channels::get_output_scaled(SRV_Channel::k_rudder) == 0) {
// trim differential spoilers if no rudder input
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_dspoilerLeft1);
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_dspoilerLeft2);
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_dspoilerRight1);
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_dspoilerRight2);
}
if (SRV_Channels::get_output_scaled(SRV_Channel::k_flap_auto) == 0 &&
SRV_Channels::get_output_scaled(SRV_Channel::k_flap) == 0) {
// trim flaperons if no flap input
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_flaperon_left);
SRV_Channels::set_trim_to_servo_out_for(SRV_Channel::k_flaperon_right);
}
// now save input trims, as these have been moved to the outputs
channel_roll->set_and_save_trim();
channel_pitch->set_and_save_trim();
channel_rudder->set_and_save_trim();
}
// esc_calibration_passthrough - pass through pilot throttle to escs
void Copter::esc_calibration_passthrough()
{
#if FRAME_CONFIG != HELI_FRAME
// clear esc flag for next time
g.esc_calibrate.set_and_save(ESCCAL_NONE);
if (motors->get_pwm_type() >= AP_Motors::PWM_TYPE_ONESHOT) {
// run at full speed for oneshot ESCs (actually done on push)
motors->set_update_rate(g.rc_speed);
} else {
// reduce update rate to motors to 50Hz
motors->set_update_rate(50);
}
// send message to GCS
gcs().send_text(MAV_SEVERITY_INFO,"ESC calibration: Passing pilot throttle to ESCs");
// disable safety if requested
BoardConfig.init_safety();
// arm motors
motors->armed(true);
SRV_Channels::enable_by_mask(motors->get_motor_mask());
hal.util->set_soft_armed(true);
while(1) {
// flash LEDs
esc_calibration_notify();
// read pilot input
read_radio();
// we run at high rate to make oneshot ESCs happy. Normal ESCs
// will only see pulses at the RC_SPEED
delay(3);
// pass through to motors
hal.rcout->cork();
motors->set_throttle_passthrough_for_esc_calibration(channel_throttle->get_control_in() / 1000.0f);
hal.rcout->push();
}
#endif // FRAME_CONFIG != HELI_FRAME
}
// esc_calibration_passthrough - pass through pilot throttle to escs
void Copter::esc_calibration_passthrough()
{
#if FRAME_CONFIG != HELI_FRAME
// clear esc flag for next time
g.esc_calibrate.set_and_save(ESCCAL_NONE);
if (motors->get_pwm_type() >= AP_Motors::PWM_TYPE_ONESHOT) {
// run at full speed for oneshot ESCs (actually done on push)
motors->set_update_rate(g.rc_speed);
} else {
// reduce update rate to motors to 50Hz
motors->set_update_rate(50);
}
// send message to GCS
gcs_send_text(MAV_SEVERITY_INFO,"ESC calibration: Passing pilot throttle to ESCs");
// arm motors
motors->armed(true);
motors->enable();
uint32_t last_notify_update_ms = 0;
while(1) {
// flash LEDS
AP_Notify::flags.esc_calibration = true;
uint32_t now = AP_HAL::millis();
if (now - last_notify_update_ms > 20) {
last_notify_update_ms = now;
update_notify();
}
// read pilot input
read_radio();
// we run at high rate do make oneshot ESCs happy. Normal ESCs
// will only see pulses at the RC_SPEED
delay(3);
// pass through to motors
motors->set_throttle_passthrough_for_esc_calibration(channel_throttle->get_control_in() / 1000.0f);
}
#endif // FRAME_CONFIG != HELI_FRAME
}
int8_t Plane::test_radio(uint8_t argc, const Menu::arg *argv)
{
print_hit_enter();
hal.scheduler->delay(1000);
// read the radio to set trims
// ---------------------------
trim_radio();
while(1) {
hal.scheduler->delay(20);
read_radio();
channel_roll->calc_pwm();
channel_pitch->calc_pwm();
channel_throttle->calc_pwm();
channel_rudder->calc_pwm();
// write out the servo PWM values
// ------------------------------
set_servos();
cliSerial->printf_P(PSTR("IN 1: %d\t2: %d\t3: %d\t4: %d\t5: %d\t6: %d\t7: %d\t8: %d\n"),
(int)channel_roll->control_in,
(int)channel_pitch->control_in,
(int)channel_throttle->control_in,
(int)channel_rudder->control_in,
(int)g.rc_5.control_in,
(int)g.rc_6.control_in,
(int)g.rc_7.control_in,
(int)g.rc_8.control_in);
if(cliSerial->available() > 0) {
return (0);
}
}
}
void Copter::rc_loop()
{
// Read radio and 3-position switch on radio
// -----------------------------------------
read_radio();
read_control_switch();
/*******************************************
* 添加者:程志强
* 描述:首先向两个舵机发送指令，然后接受数据，并向日志中书写数据
* 修改日期：2016/5/5,2016/6/24
* 频率提高到400Hz
******************************************* */
/*******************************************
* 添加者:程志强
* 描述:首先向两个舵机发送指令，然后接受数据，并向日志中书写数据
* 修改日期：2016/6/24
******************************************* */
chuart.send_token();
chuart.readUart();
DataFlash.Log_Write_Act(chuart.sd[0],0);
DataFlash.Log_Write_Act(chuart.sd[1],1);
}
// check if we should enter esc calibration mode
void Copter::esc_calibration_startup_check()
{
#if FRAME_CONFIG != HELI_FRAME
// delay up to 2 second for first radio input
uint8_t i = 0;
while ((i++ < 100) && (last_radio_update_ms == 0)) {
delay(20);
read_radio();
}
// exit immediately if pre-arm rc checks fail
arming.pre_arm_rc_checks(true);
if (!ap.pre_arm_rc_check) {
// clear esc flag for next time
if ((g.esc_calibrate != ESCCAL_NONE) && (g.esc_calibrate != ESCCAL_DISABLED)) {
g.esc_calibrate.set_and_save(ESCCAL_NONE);
}
return;
}
// check ESC parameter
switch (g.esc_calibrate) {
case ESCCAL_NONE:
// check if throttle is high
if (channel_throttle->get_control_in() >= ESC_CALIBRATION_HIGH_THROTTLE) {
// we will enter esc_calibrate mode on next reboot
g.esc_calibrate.set_and_save(ESCCAL_PASSTHROUGH_IF_THROTTLE_HIGH);
// send message to gcs
gcs_send_text(MAV_SEVERITY_CRITICAL,"ESC calibration: Restart board");
// turn on esc calibration notification
AP_Notify::flags.esc_calibration = true;
// block until we restart
while(1) { delay(5); }
}
break;
case ESCCAL_PASSTHROUGH_IF_THROTTLE_HIGH:
// check if throttle is high
if (channel_throttle->get_control_in() >= ESC_CALIBRATION_HIGH_THROTTLE) {
// pass through pilot throttle to escs
esc_calibration_passthrough();
}
break;
case ESCCAL_PASSTHROUGH_ALWAYS:
// pass through pilot throttle to escs
esc_calibration_passthrough();
break;
case ESCCAL_AUTO:
// perform automatic ESC calibration
esc_calibration_auto();
break;
case ESCCAL_DISABLED:
default:
// do nothing
break;
}
// clear esc flag for next time
if (g.esc_calibrate != ESCCAL_DISABLED) {
g.esc_calibrate.set_and_save(ESCCAL_NONE);
}
#endif // FRAME_CONFIG != HELI_FRAME
}
// 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
}