ardupilot/ArduCopter/esc_calibration.cpp
Randy Mackay 36327d56de Copter: reject reboot request from GCS if auto esc cal on next reboot
this resolves an edge case in which the motors could spin up on the next reboot because the user didn't unplug the battery to reboot the flight controller
2019-10-15 07:41:44 +09:00

184 lines
6.0 KiB
C++

#include "Copter.h"
/*****************************************************************************
* Functions to check and perform ESC calibration
*****************************************************************************/
#define ESC_CALIBRATION_HIGH_THROTTLE 950
// check if we should enter esc calibration mode
void Copter::esc_calibration_startup_check()
{
if (motors->get_pwm_type() == AP_Motors::PWM_TYPE_BRUSHED) {
// ESC cal not valid for brushed motors
return;
}
#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)) {
hal.scheduler->delay(20);
read_radio();
}
// exit immediately if pre-arm rc checks fail
if (!arming.rc_calibration_checks(true)) {
// clear esc flag for next time
if ((g.esc_calibrate != ESCCalibrationModes::ESCCAL_NONE) && (g.esc_calibrate != ESCCalibrationModes::ESCCAL_DISABLED)) {
g.esc_calibrate.set_and_save(ESCCalibrationModes::ESCCAL_NONE);
}
return;
}
// check ESC parameter
switch (g.esc_calibrate) {
case ESCCalibrationModes::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(ESCCalibrationModes::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) { hal.scheduler->delay(5); }
}
break;
case ESCCalibrationModes::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 ESCCalibrationModes::ESCCAL_PASSTHROUGH_ALWAYS:
// pass through pilot throttle to escs
esc_calibration_passthrough();
break;
case ESCCalibrationModes::ESCCAL_AUTO:
// perform automatic ESC calibration
esc_calibration_auto();
break;
case ESCCalibrationModes::ESCCAL_DISABLED:
default:
// do nothing
break;
}
// clear esc flag for next time
if (g.esc_calibrate != ESCCalibrationModes::ESCCAL_DISABLED) {
g.esc_calibrate.set_and_save(ESCCalibrationModes::ESCCAL_NONE);
}
#endif // FRAME_CONFIG != HELI_FRAME
}
// esc_calibration_passthrough - pass through pilot throttle to escs
void Copter::esc_calibration_passthrough()
{
#if FRAME_CONFIG != HELI_FRAME
// send message to GCS
gcs().send_text(MAV_SEVERITY_INFO,"ESC calibration: Passing pilot throttle to ESCs");
esc_calibration_setup();
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
hal.scheduler->delay(3);
// pass through to motors
SRV_Channels::cork();
motors->set_throttle_passthrough_for_esc_calibration(channel_throttle->get_control_in() / 1000.0f);
SRV_Channels::push();
}
#endif // FRAME_CONFIG != HELI_FRAME
}
// esc_calibration_auto - calibrate the ESCs automatically using a timer and no pilot input
void Copter::esc_calibration_auto()
{
#if FRAME_CONFIG != HELI_FRAME
// send message to GCS
gcs().send_text(MAV_SEVERITY_INFO,"ESC calibration: Auto calibration");
esc_calibration_setup();
// raise throttle to maximum
SRV_Channels::cork();
motors->set_throttle_passthrough_for_esc_calibration(1.0f);
SRV_Channels::push();
// delay for 5 seconds while outputting pulses
uint32_t tstart = millis();
while (millis() - tstart < 5000) {
SRV_Channels::cork();
motors->set_throttle_passthrough_for_esc_calibration(1.0f);
SRV_Channels::push();
esc_calibration_notify();
hal.scheduler->delay(3);
}
// block until we restart
while(1) {
SRV_Channels::cork();
motors->set_throttle_passthrough_for_esc_calibration(0.0f);
SRV_Channels::push();
esc_calibration_notify();
hal.scheduler->delay(3);
}
#endif // FRAME_CONFIG != HELI_FRAME
}
// flash LEDs to notify the user that ESC calibration is happening
void Copter::esc_calibration_notify()
{
AP_Notify::flags.esc_calibration = true;
uint32_t now = AP_HAL::millis();
if (now - esc_calibration_notify_update_ms > 20) {
esc_calibration_notify_update_ms = now;
notify.update();
}
}
void Copter::esc_calibration_setup()
{
// 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);
}
// disable safety if requested
BoardConfig.init_safety();
// wait for safety switch to be pressed
uint32_t tstart = 0;
while (hal.util->safety_switch_state() == AP_HAL::Util::SAFETY_DISARMED) {
const uint32_t tnow = AP_HAL::millis();
if (tnow - tstart >= 5000) {
gcs().send_text(MAV_SEVERITY_INFO,"ESC calibration: Push safety switch");
tstart = tnow;
}
esc_calibration_notify();
hal.scheduler->delay(3);
}
// arm and enable motors
motors->armed(true);
SRV_Channels::enable_by_mask(motors->get_motor_mask());
hal.util->set_soft_armed(true);
}