2015-05-29 23:12:49 -03:00
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#include "Copter.h"
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2013-11-03 01:26:19 -04:00
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// Traditional helicopter variables and functions
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#if FRAME_CONFIG == HELI_FRAME
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#ifndef HELI_DYNAMIC_FLIGHT_SPEED_MIN
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2017-10-25 01:27:25 -03:00
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#define HELI_DYNAMIC_FLIGHT_SPEED_MIN 500 // we are in "dynamic flight" when the speed is over 5m/s for 2 seconds
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2013-11-03 01:26:19 -04:00
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#endif
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// counter to control dynamic flight profile
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static int8_t heli_dynamic_flight_counter;
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2013-11-10 08:05:58 -04:00
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// heli_init - perform any special initialisation required for the tradheli
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2015-05-29 23:12:49 -03:00
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void Copter::heli_init()
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2013-11-10 08:05:58 -04:00
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{
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2015-10-12 22:05:49 -03:00
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// pre-load stab col values as mode is initialized as Stabilize, but stabilize_init() function is not run on start-up.
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input_manager.set_use_stab_col(true);
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input_manager.set_stab_col_ramp(1.0);
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2013-11-09 01:25:06 -04:00
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}
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2013-11-03 01:26:19 -04:00
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// heli_check_dynamic_flight - updates the dynamic_flight flag based on our horizontal velocity
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// should be called at 50hz
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2015-05-29 23:12:49 -03:00
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void Copter::check_dynamic_flight(void)
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2013-11-03 01:26:19 -04:00
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{
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2019-04-09 09:16:58 -03:00
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if (motors->get_spool_state() != AP_Motors::SpoolState::THROTTLE_UNLIMITED ||
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2019-09-07 20:33:56 -03:00
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control_mode == Mode::Number::LAND || (control_mode==Mode::Number::RTL && mode_rtl.state() == RTL_Land) || (control_mode == Mode::Number::AUTO && mode_auto.mode() == Auto_Land)) {
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2013-11-03 01:26:19 -04:00
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heli_dynamic_flight_counter = 0;
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heli_flags.dynamic_flight = false;
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return;
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}
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bool moving = false;
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// with GPS lock use inertial nav to determine if we are moving
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2015-01-02 07:43:50 -04:00
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if (position_ok()) {
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2017-10-13 00:42:09 -03:00
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// get horizontal speed
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const float speed = inertial_nav.get_speed_xy();
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moving = (speed >= HELI_DYNAMIC_FLIGHT_SPEED_MIN);
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2013-11-03 01:26:19 -04:00
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}else{
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// with no GPS lock base it on throttle and forward lean angle
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2017-01-09 03:31:26 -04:00
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moving = (motors->get_throttle() > 0.8f || ahrs.pitch_sensor < -1500);
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2013-11-03 01:26:19 -04:00
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}
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2017-02-09 07:30:59 -04:00
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if (!moving && rangefinder_state.enabled && rangefinder.status_orient(ROTATION_PITCH_270) == RangeFinder::RangeFinder_Good) {
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2015-09-03 23:06:00 -03:00
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// when we are more than 2m from the ground with good
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// rangefinder lock consider it to be dynamic flight
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2017-02-09 07:30:59 -04:00
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moving = (rangefinder.distance_cm_orient(ROTATION_PITCH_270) > 200);
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2015-09-03 23:06:00 -03:00
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}
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2013-11-03 01:26:19 -04:00
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if (moving) {
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// if moving for 2 seconds, set the dynamic flight flag
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if (!heli_flags.dynamic_flight) {
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heli_dynamic_flight_counter++;
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if (heli_dynamic_flight_counter >= 100) {
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heli_flags.dynamic_flight = true;
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heli_dynamic_flight_counter = 100;
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}
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}
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}else{
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// if not moving for 2 seconds, clear the dynamic flight flag
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if (heli_flags.dynamic_flight) {
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if (heli_dynamic_flight_counter > 0) {
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heli_dynamic_flight_counter--;
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}else{
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heli_flags.dynamic_flight = false;
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}
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}
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}
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}
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2014-05-09 18:07:52 -03:00
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// update_heli_control_dynamics - pushes several important factors up into AP_MotorsHeli.
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// should be run between the rate controller and the servo updates.
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2015-05-29 23:12:49 -03:00
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void Copter::update_heli_control_dynamics(void)
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2014-05-09 18:07:52 -03:00
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{
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// Use Leaky_I if we are not moving fast
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2017-01-09 03:31:26 -04:00
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attitude_control->use_leaky_i(!heli_flags.dynamic_flight);
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2015-10-23 19:41:01 -03:00
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2017-01-09 03:31:26 -04:00
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if (ap.land_complete || (is_zero(motors->get_desired_rotor_speed()))){
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2015-10-23 19:41:01 -03:00
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// if we are landed or there is no rotor power demanded, decrement slew scalar
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hover_roll_trim_scalar_slew--;
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} else {
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// if we are not landed and motor power is demanded, increment slew scalar
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hover_roll_trim_scalar_slew++;
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}
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2016-06-04 22:21:31 -03:00
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hover_roll_trim_scalar_slew = constrain_int16(hover_roll_trim_scalar_slew, 0, scheduler.get_loop_rate_hz());
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2015-10-23 19:41:01 -03:00
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// set hover roll trim scalar, will ramp from 0 to 1 over 1 second after we think helicopter has taken off
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2018-11-16 11:48:42 -04:00
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attitude_control->set_hover_roll_trim_scalar((float) hover_roll_trim_scalar_slew/(float) scheduler.get_loop_rate_hz());
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2014-05-09 18:07:52 -03:00
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}
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2013-11-06 08:39:39 -04:00
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// heli_update_landing_swash - sets swash plate flag so higher minimum is used when landed or landing
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// should be called soon after update_land_detector in main code
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2015-05-29 23:12:49 -03:00
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void Copter::heli_update_landing_swash()
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2013-11-06 08:39:39 -04:00
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{
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2018-12-23 22:18:10 -04:00
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switch (control_mode) {
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2019-09-07 20:33:56 -03:00
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case Mode::Number::ACRO:
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case Mode::Number::STABILIZE:
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case Mode::Number::DRIFT:
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case Mode::Number::SPORT:
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2013-11-06 08:39:39 -04:00
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// manual modes always uses full swash range
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2017-01-09 03:31:26 -04:00
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motors->set_collective_for_landing(false);
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2013-11-06 08:39:39 -04:00
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break;
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2019-09-07 20:33:56 -03:00
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case Mode::Number::LAND:
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2013-11-06 08:39:39 -04:00
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// landing always uses limit swash range
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2017-01-09 03:31:26 -04:00
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motors->set_collective_for_landing(true);
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2013-11-06 08:39:39 -04:00
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break;
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2019-09-07 20:33:56 -03:00
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case Mode::Number::RTL:
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case Mode::Number::SMART_RTL:
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2017-12-11 01:43:27 -04:00
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if (mode_rtl.state() == RTL_Land) {
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2017-01-09 03:31:26 -04:00
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motors->set_collective_for_landing(true);
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2014-02-03 08:06:34 -04:00
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}else{
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2017-01-09 03:31:26 -04:00
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motors->set_collective_for_landing(!heli_flags.dynamic_flight || ap.land_complete || !ap.auto_armed);
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2014-02-03 08:06:34 -04:00
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}
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break;
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2019-09-07 20:33:56 -03:00
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case Mode::Number::AUTO:
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2017-12-11 01:43:27 -04:00
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if (mode_auto.mode() == Auto_Land) {
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2017-01-09 03:31:26 -04:00
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motors->set_collective_for_landing(true);
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2014-02-03 08:06:34 -04:00
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}else{
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2017-01-09 03:31:26 -04:00
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motors->set_collective_for_landing(!heli_flags.dynamic_flight || ap.land_complete || !ap.auto_armed);
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2014-02-03 08:06:34 -04:00
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}
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break;
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2013-11-06 08:39:39 -04:00
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default:
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// auto and hold use limited swash when landed
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2017-01-09 03:31:26 -04:00
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motors->set_collective_for_landing(!heli_flags.dynamic_flight || ap.land_complete || !ap.auto_armed);
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2013-11-06 08:39:39 -04:00
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break;
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}
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}
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2013-11-08 04:29:54 -04:00
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// heli_update_rotor_speed_targets - reads pilot input and passes new rotor speed targets to heli motors object
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2015-05-29 23:12:49 -03:00
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void Copter::heli_update_rotor_speed_targets()
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2013-11-08 04:29:54 -04:00
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{
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2015-06-16 23:00:48 -03:00
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static bool rotor_runup_complete_last = false;
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2013-11-08 04:29:54 -04:00
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// get rotor control method
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2017-01-09 03:31:26 -04:00
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uint8_t rsc_control_mode = motors->get_rsc_mode();
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2019-01-26 10:33:32 -04:00
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float rsc_control_deglitched = 0.0f;
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2019-04-03 13:25:47 -03:00
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RC_Channel *rc_ptr = rc().find_channel_for_option(RC_Channel::AUX_FUNC::MOTOR_INTERLOCK);
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2019-01-26 10:33:32 -04:00
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if (rc_ptr != nullptr) {
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rsc_control_deglitched = rotor_speed_deglitch_filter.apply((float)rc_ptr->get_control_in()) * 0.001f;
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}
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2015-08-12 19:57:33 -03:00
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switch (rsc_control_mode) {
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2015-08-28 03:23:58 -03:00
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case ROTOR_CONTROL_MODE_SPEED_PASSTHROUGH:
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2019-02-09 19:58:42 -04:00
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// pass through pilot desired rotor speed from the RC
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2019-01-26 10:33:32 -04:00
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if (motors->get_interlock()) {
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2017-01-09 03:31:26 -04:00
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motors->set_desired_rotor_speed(rsc_control_deglitched);
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2015-08-12 19:57:33 -03:00
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} else {
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2017-01-09 03:31:26 -04:00
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motors->set_desired_rotor_speed(0.0f);
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2015-08-12 19:57:33 -03:00
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}
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break;
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2015-08-28 03:23:58 -03:00
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case ROTOR_CONTROL_MODE_SPEED_SETPOINT:
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case ROTOR_CONTROL_MODE_OPEN_LOOP_POWER_OUTPUT:
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case ROTOR_CONTROL_MODE_CLOSED_LOOP_POWER_OUTPUT:
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2019-02-09 19:58:42 -04:00
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// pass setpoint through as desired rotor speed. Needs work, this is pointless as it is
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// not used by closed loop control. Being used as a catch-all for other modes regardless
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// of whether or not they actually use it
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// set rpm from rotor speed sensor
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2019-01-26 10:33:32 -04:00
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if (motors->get_interlock()) {
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2019-06-05 21:21:41 -03:00
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#if RPM_ENABLED == ENABLED
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2019-02-09 19:58:42 -04:00
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motors->set_rpm(rpm_sensor.get_rpm(0));
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2019-06-05 21:21:41 -03:00
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#endif
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2017-01-09 03:31:26 -04:00
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motors->set_desired_rotor_speed(motors->get_rsc_setpoint());
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2015-08-12 19:57:33 -03:00
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}else{
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2017-01-09 03:31:26 -04:00
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motors->set_desired_rotor_speed(0.0f);
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2015-08-12 19:57:33 -03:00
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}
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break;
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2013-11-08 04:29:54 -04:00
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}
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2015-06-16 23:00:48 -03:00
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// when rotor_runup_complete changes to true, log event
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2017-01-09 03:31:26 -04:00
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if (!rotor_runup_complete_last && motors->rotor_runup_complete()){
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2015-06-16 23:00:48 -03:00
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Log_Write_Event(DATA_ROTOR_RUNUP_COMPLETE);
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2017-01-09 03:31:26 -04:00
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} else if (rotor_runup_complete_last && !motors->rotor_runup_complete()){
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2015-06-18 20:39:58 -03:00
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Log_Write_Event(DATA_ROTOR_SPEED_BELOW_CRITICAL);
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2015-06-16 23:00:48 -03:00
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}
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2017-01-09 03:31:26 -04:00
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rotor_runup_complete_last = motors->rotor_runup_complete();
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2013-11-08 04:29:54 -04:00
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}
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2019-11-28 16:21:07 -04:00
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// heli_update_autorotation - determines if aircraft is in autorotation and sets motors flag and switches
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// to autorotation flight mode if manual collective is not being used.
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void Copter::heli_update_autorotation()
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{
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#if MODE_AUTOROTATE_ENABLED == ENABLED
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//set autonomous autorotation flight mode
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if (!ap.land_complete && !motors->get_interlock() && !flightmode->has_manual_throttle() && g2.arot.is_enable()) {
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heli_flags.in_autorotation = true;
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set_mode(Mode::Number::AUTOROTATE, ModeReason::AUTOROTATION_START);
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} else {
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heli_flags.in_autorotation = false;
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}
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// sets autorotation flags through out libraries
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heli_set_autorotation(heli_flags.in_autorotation);
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if (!ap.land_complete && g2.arot.is_enable()) {
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motors->set_enable_bailout(true);
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} else {
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motors->set_enable_bailout(false);
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}
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#else
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heli_flags.in_autorotation = false;
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motors->set_enable_bailout(false);
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#endif
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}
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#if MODE_AUTOROTATE_ENABLED == ENABLED
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// heli_set_autorotation - set the autorotation f`lag throughout libraries
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void Copter::heli_set_autorotation(bool autorotation)
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{
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motors->set_in_autorotation(autorotation);
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}
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#endif
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2014-01-13 04:23:09 -04:00
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#endif // FRAME_CONFIG == HELI_FRAME
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