// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #include "Copter.h" /***************************************************************************** * esc_calibration.pde : functions to check and perform ESC calibration *****************************************************************************/ #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 }; // check if we should enter esc calibration mode void Copter::esc_calibration_startup_check() { // 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.set_and_save(ESCCAL_NONE); } return; } // check ESC parameter switch (g.esc_calibrate) { case ESCCAL_NONE: // check if throttle is high if (channel_throttle->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_P(SEVERITY_HIGH,PSTR("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->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; default: // do nothing break; } // clear esc flag for next time g.esc_calibrate.set_and_save(ESCCAL_NONE); } // esc_calibration_passthrough - pass through pilot throttle to escs void Copter::esc_calibration_passthrough() { // 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(SEVERITY_HIGH,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); } } // esc_calibration_auto - calibrate the ESCs automatically using a timer and no pilot input void Copter::esc_calibration_auto() { bool printed_msg = false; // reduce update rate to motors to 50Hz motors.set_update_rate(50); // send message to GCS gcs_send_text_P(SEVERITY_HIGH,PSTR("ESC Calibration: auto calibration")); // arm and enable motors motors.armed(true); motors.enable(); // flash LEDS AP_Notify::flags.esc_calibration = true; // raise throttle to maximum delay(10); motors.throttle_pass_through(channel_throttle->radio_max); // wait for safety switch to be pressed while (hal.util->safety_switch_state() == AP_HAL::Util::SAFETY_DISARMED) { if (!printed_msg) { gcs_send_text_P(SEVERITY_HIGH,PSTR("ESC Calibration: push safety switch")); printed_msg = true; } delay(10); } // delay for 5 seconds delay(5000); // reduce throttle to minimum motors.throttle_pass_through(channel_throttle->radio_min); // clear esc parameter g.esc_calibrate.set_and_save(ESCCAL_NONE); // block until we restart while(1) { delay(5); } }