/// -*- tab-width: 4; Mode: C++; c-basic-offset: 4; indent-tabs-mode: nil -*- #define ARM_DELAY 10 // one secon #define DISARM_DELAY 10 // one secon #define LEVEL_DELAY 120 // twelve seconds #define AUTO_LEVEL_DELAY 150 // twentyfive seconds // called at 10hz static void arm_motors() { static int arming_counter; // Arm motor output : Throttle down and full yaw right for more than 2 seconds if (g.rc_3.control_in == 0){ // full right if (g.rc_4.control_in > 4000) { // don't allow arming in anything but manual if (control_mode < ALT_HOLD){ if (arming_counter > AUTO_LEVEL_DELAY){ auto_level_counter = 155; arming_counter = 0; }else if (arming_counter == ARM_DELAY){ #if HIL_MODE != HIL_MODE_DISABLED hil.send_text_P(SEVERITY_HIGH, PSTR("ARMING MOTORS")); #endif motor_armed = true; arming_counter = ARM_DELAY; // Tune down DCM // ------------------- #if HIL_MODE != HIL_MODE_ATTITUDE dcm.kp_roll_pitch(0.030000); dcm.ki_roll_pitch(0.00001278), // 50 hz I term //dcm.ki_roll_pitch(0.000006); #endif // tune down compass // ----------------- dcm.kp_yaw(0.08); dcm.ki_yaw(0); // Remember Orientation // -------------------- init_simple_bearing(); // Reset home position // ---------------------- if(home_is_set) init_home(); if(did_ground_start == false){ did_ground_start = true; startup_ground(); } #if HIL_MODE != HIL_MODE_ATTITUDE // read Baro pressure at ground - // this resets Baro for more accuracy //----------------------------------- init_barometer(); #endif // temp hack motor_light = true; digitalWrite(A_LED_PIN, HIGH); arming_counter++; } else{ arming_counter++; } } // full left }else if (g.rc_4.control_in < -4000) { //Serial.print(arming_counter, DEC); if (arming_counter > LEVEL_DELAY){ //Serial.print("init"); imu.init_accel(mavlink_delay); arming_counter = 0; }else if (arming_counter == DISARM_DELAY){ #if HIL_MODE != HIL_MODE_DISABLED hil.send_text_P(SEVERITY_HIGH, PSTR("DISARMING MOTORS")); #endif motor_armed = false; arming_counter = DISARM_DELAY; compass.save_offsets(); // Tune down DCM // ------------------- #if HIL_MODE != HIL_MODE_ATTITUDE dcm.kp_roll_pitch(0.12); // higher for fast recovery //dcm.ki_roll_pitch(0.00000319); // 1/4 of the normal rate for 200 hz loop #endif // tune up compass // ----------------- dcm.kp_yaw(0.8); dcm.ki_yaw(0.00004); // Clear throttle slew // ------------------- //throttle_slew = 0; arming_counter++; }else{ arming_counter++; } // centered }else{ arming_counter = 0; } }else{ arming_counter = 0; } } /***************************************** * Set the flight control servos based on the current calculated values *****************************************/ static void set_servos_4() { if (motor_armed == true && motor_auto_armed == true) { // creates the radio_out and pwm_out values output_motors_armed(); } else{ output_motors_disarmed(); } }