ardupilot/ArduCopter/esc_calibration.cpp

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// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*-
#include "Copter.h"
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/*****************************************************************************
* Functions to check and perform ESC calibration
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*****************************************************************************/
#define ESC_CALIBRATION_HIGH_THROTTLE 950
// enum for ESC CALIBRATION
enum ESCCalibrationModes {
ESCCAL_NONE = 0,
ESCCAL_PASSTHROUGH_IF_THROTTLE_HIGH = 1,
ESCCAL_PASSTHROUGH_ALWAYS = 2,
ESCCAL_AUTO = 3,
ESCCAL_DISABLED = 9,
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};
// check if we should enter esc calibration mode
void Copter::esc_calibration_startup_check()
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{
#if FRAME_CONFIG != HELI_FRAME
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// exit immediately if pre-arm rc checks fail
pre_arm_rc_checks();
if (!ap.pre_arm_rc_check) {
// clear esc flag for next time
if ((g.esc_calibrate != ESCCAL_NONE) && (g.esc_calibrate != ESCCAL_DISABLED)) {
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g.esc_calibrate.set_and_save(ESCCAL_NONE);
}
return;
}
// check ESC parameter
switch (g.esc_calibrate) {
case ESCCAL_NONE:
// check if throttle is high
ArduCopter: Fix up after refactoring RC_Channel class Further to refactor of RC_Channel class which included adding get_xx set_xx methods, change reads and writes to the public members to calls to get and set functionsss old public member(int16_t) get function -> int16_t set function (int16_t) (expression where c is an object of type RC_Channel) c.radio_in c.get_radio_in() c.set_radio_in(v) c.control_in c.get_control_in() c.set_control_in(v) c.servo_out c.get_servo_out() c.set_servo_out(v) c.pwm_out c.get_pwm_out() // use existing c.radio_out c.get_radio_out() c.set_radio_out(v) c.radio_max c.get_radio_max() c.set_radio_max(v) c.radio_min c.get_radio_min() c.set_radio_min(v) c.radio_trim c.get_radio_trim() c.set_radio_trim(v); c.min_max_configured() // return true if min and max are configured Because data members of RC_Channels are now private and so cannot be written directly some overloads are provided in the Plane classes to provide the old functionality new overload Plane::stick_mix_channel(RC_Channel *channel) which forwards to the previously existing void stick_mix_channel(RC_Channel *channel, int16_t &servo_out); new overload Plane::channel_output_mixer(Rc_Channel* , RC_Channel*)const which forwards to (uint8_t mixing_type, int16_t & chan1, int16_t & chan2)const; Rename functions RC_Channel_aux::set_radio_trim(Aux_servo_function_t function) to RC_Channel_aux::set_trim_to_radio_in_for(Aux_servo_function_t function) RC_Channel_aux::set_servo_out(Aux_servo_function_t function, int16_t value) to RC_Channel_aux::set_servo_out_for(Aux_servo_function_t function, int16_t value) Rationale: RC_Channel is a complicated class, which combines several functionalities dealing with stick inputs in pwm and logical units, logical and actual actuator outputs, unit conversion etc, etc The intent of this PR is to clarify existing use of the class. At the basic level it should now be possible to grep all places where private variable is set by searching for the set_xx function. (The wider purpose is to provide a more generic and logically simpler method of output mixing. This is a small step)
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if (channel_throttle->get_control_in() >= ESC_CALIBRATION_HIGH_THROTTLE) {
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// 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");
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// 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
ArduCopter: Fix up after refactoring RC_Channel class Further to refactor of RC_Channel class which included adding get_xx set_xx methods, change reads and writes to the public members to calls to get and set functionsss old public member(int16_t) get function -> int16_t set function (int16_t) (expression where c is an object of type RC_Channel) c.radio_in c.get_radio_in() c.set_radio_in(v) c.control_in c.get_control_in() c.set_control_in(v) c.servo_out c.get_servo_out() c.set_servo_out(v) c.pwm_out c.get_pwm_out() // use existing c.radio_out c.get_radio_out() c.set_radio_out(v) c.radio_max c.get_radio_max() c.set_radio_max(v) c.radio_min c.get_radio_min() c.set_radio_min(v) c.radio_trim c.get_radio_trim() c.set_radio_trim(v); c.min_max_configured() // return true if min and max are configured Because data members of RC_Channels are now private and so cannot be written directly some overloads are provided in the Plane classes to provide the old functionality new overload Plane::stick_mix_channel(RC_Channel *channel) which forwards to the previously existing void stick_mix_channel(RC_Channel *channel, int16_t &servo_out); new overload Plane::channel_output_mixer(Rc_Channel* , RC_Channel*)const which forwards to (uint8_t mixing_type, int16_t & chan1, int16_t & chan2)const; Rename functions RC_Channel_aux::set_radio_trim(Aux_servo_function_t function) to RC_Channel_aux::set_trim_to_radio_in_for(Aux_servo_function_t function) RC_Channel_aux::set_servo_out(Aux_servo_function_t function, int16_t value) to RC_Channel_aux::set_servo_out_for(Aux_servo_function_t function, int16_t value) Rationale: RC_Channel is a complicated class, which combines several functionalities dealing with stick inputs in pwm and logical units, logical and actual actuator outputs, unit conversion etc, etc The intent of this PR is to clarify existing use of the class. At the basic level it should now be possible to grep all places where private variable is set by searching for the set_xx function. (The wider purpose is to provide a more generic and logically simpler method of output mixing. This is a small step)
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if (channel_throttle->get_control_in() >= ESC_CALIBRATION_HIGH_THROTTLE) {
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// 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:
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default:
// do nothing
break;
}
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// 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
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}
// esc_calibration_passthrough - pass through pilot throttle to escs
void Copter::esc_calibration_passthrough()
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{
#if FRAME_CONFIG != HELI_FRAME
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// 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(MAV_SEVERITY_INFO,"ESC calibration: Passing pilot throttle to ESCs");
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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.set_throttle_passthrough_for_esc_calibration(channel_throttle->get_control_in() / 1000.0f);
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}
#endif // FRAME_CONFIG != HELI_FRAME
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}
// esc_calibration_auto - calibrate the ESCs automatically using a timer and no pilot input
void Copter::esc_calibration_auto()
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{
#if FRAME_CONFIG != HELI_FRAME
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bool printed_msg = false;
// reduce update rate to motors to 50Hz
motors.set_update_rate(50);
// send message to GCS
gcs_send_text(MAV_SEVERITY_INFO,"ESC calibration: Auto calibration");
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// arm and enable motors
motors.armed(true);
motors.enable();
// flash LEDS
AP_Notify::flags.esc_calibration = true;
// raise throttle to maximum
delay(10);
motors.set_throttle_passthrough_for_esc_calibration(1.0f);
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// wait for safety switch to be pressed
while (hal.util->safety_switch_state() == AP_HAL::Util::SAFETY_DISARMED) {
if (!printed_msg) {
gcs_send_text(MAV_SEVERITY_INFO,"ESC calibration: Push safety switch");
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printed_msg = true;
}
delay(10);
}
// delay for 5 seconds
delay(5000);
// reduce throttle to minimum
motors.set_throttle_passthrough_for_esc_calibration(0.0f);
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// clear esc parameter
g.esc_calibrate.set_and_save(ESCCAL_NONE);
// block until we restart
while(1) { delay(5); }
#endif // FRAME_CONFIG != HELI_FRAME
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}