mirror of
https://github.com/ArduPilot/ardupilot
synced 2025-01-02 14:13:42 -04:00
2425c65e74
this implements what betaflight calls 'air-mode'. This gives attitude control when throttle is at zero, allowing for zero-throttle maneuvers, plus keeping the copter level on the ground. This was already implemented if an interlock switch was setup, but it should also work with an arming switch. If using an arming switch then throttle should not be considered zero as long as the arming switch hasn't gone low.
212 lines
7.9 KiB
C++
212 lines
7.9 KiB
C++
#include "Copter.h"
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// Function that will read the radio data, limit servos and trigger a failsafe
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// ----------------------------------------------------------------------------
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void Copter::default_dead_zones()
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{
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channel_roll->set_default_dead_zone(20);
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channel_pitch->set_default_dead_zone(20);
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#if FRAME_CONFIG == HELI_FRAME
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channel_throttle->set_default_dead_zone(10);
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channel_yaw->set_default_dead_zone(15);
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RC_Channels::rc_channel(CH_6)->set_default_dead_zone(10);
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#else
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channel_throttle->set_default_dead_zone(30);
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channel_yaw->set_default_dead_zone(20);
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#endif
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RC_Channels::rc_channel(CH_6)->set_default_dead_zone(0);
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}
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void Copter::init_rc_in()
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{
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channel_roll = RC_Channels::rc_channel(rcmap.roll()-1);
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channel_pitch = RC_Channels::rc_channel(rcmap.pitch()-1);
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channel_throttle = RC_Channels::rc_channel(rcmap.throttle()-1);
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channel_yaw = RC_Channels::rc_channel(rcmap.yaw()-1);
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// set rc channel ranges
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channel_roll->set_angle(ROLL_PITCH_YAW_INPUT_MAX);
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channel_pitch->set_angle(ROLL_PITCH_YAW_INPUT_MAX);
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channel_yaw->set_angle(ROLL_PITCH_YAW_INPUT_MAX);
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channel_throttle->set_range(1000);
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//set auxiliary servo ranges
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RC_Channels::rc_channel(CH_5)->set_range(1000);
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RC_Channels::rc_channel(CH_6)->set_range(1000);
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RC_Channels::rc_channel(CH_7)->set_range(1000);
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RC_Channels::rc_channel(CH_8)->set_range(1000);
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// set default dead zones
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default_dead_zones();
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// initialise throttle_zero flag
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ap.throttle_zero = true;
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// Allow override by default at start
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ap.rc_override_enable = true;
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}
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// init_rc_out -- initialise motors and check if pilot wants to perform ESC calibration
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void Copter::init_rc_out()
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{
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motors->set_loop_rate(scheduler.get_loop_rate_hz());
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motors->init((AP_Motors::motor_frame_class)g2.frame_class.get(), (AP_Motors::motor_frame_type)g.frame_type.get());
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// enable aux servos to cope with multiple output channels per motor
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SRV_Channels::enable_aux_servos();
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// update rate must be set after motors->init() to allow for motor mapping
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motors->set_update_rate(g.rc_speed);
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#if FRAME_CONFIG != HELI_FRAME
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motors->set_throttle_range(channel_throttle->get_radio_min(), channel_throttle->get_radio_max());
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#else
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// setup correct scaling for ESCs like the UAVCAN PX4ESC which
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// take a proportion of speed.
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hal.rcout->set_esc_scaling(channel_throttle->get_radio_min(), channel_throttle->get_radio_max());
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#endif
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// refresh auxiliary channel to function map
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SRV_Channels::update_aux_servo_function();
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#if FRAME_CONFIG != HELI_FRAME
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/*
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setup a default safety ignore mask, so that servo gimbals can be active while safety is on
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*/
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uint16_t safety_ignore_mask = (~copter.motors->get_motor_mask()) & 0x3FFF;
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BoardConfig.set_default_safety_ignore_mask(safety_ignore_mask);
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#endif
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// check if we should enter esc calibration mode
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esc_calibration_startup_check();
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}
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// enable_motor_output() - enable and output lowest possible value to motors
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void Copter::enable_motor_output()
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{
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// enable motors
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motors->output_min();
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}
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void Copter::read_radio()
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{
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uint32_t tnow_ms = millis();
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if (RC_Channels::read_input()) {
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ap.new_radio_frame = true;
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set_throttle_and_failsafe(channel_throttle->get_radio_in());
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set_throttle_zero_flag(channel_throttle->get_control_in());
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// flag we must have an rc receiver attached
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if (!failsafe.rc_override_active) {
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ap.rc_receiver_present = true;
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}
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// pass pilot input through to motors (used to allow wiggling servos while disarmed on heli, single, coax copters)
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radio_passthrough_to_motors();
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float dt = (tnow_ms - last_radio_update_ms)*1.0e-3f;
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rc_throttle_control_in_filter.apply(channel_throttle->get_control_in(), dt);
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last_radio_update_ms = tnow_ms;
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}else{
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uint32_t elapsed = tnow_ms - last_radio_update_ms;
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// turn on throttle failsafe if no update from the RC Radio for 500ms or 2000ms if we are using RC_OVERRIDE
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if (((!failsafe.rc_override_active && (elapsed >= FS_RADIO_TIMEOUT_MS)) || (failsafe.rc_override_active && (elapsed >= FS_RADIO_RC_OVERRIDE_TIMEOUT_MS))) &&
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(g.failsafe_throttle && (ap.rc_receiver_present||motors->armed()) && !failsafe.radio)) {
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Log_Write_Error(ERROR_SUBSYSTEM_RADIO, ERROR_CODE_RADIO_LATE_FRAME);
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set_failsafe_radio(true);
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}
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}
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}
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#define FS_COUNTER 3 // radio failsafe kicks in after 3 consecutive throttle values below failsafe_throttle_value
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void Copter::set_throttle_and_failsafe(uint16_t throttle_pwm)
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{
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// if failsafe not enabled pass through throttle and exit
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if(g.failsafe_throttle == FS_THR_DISABLED) {
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channel_throttle->set_pwm(throttle_pwm);
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return;
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}
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//check for low throttle value
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if (throttle_pwm < (uint16_t)g.failsafe_throttle_value) {
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// if we are already in failsafe or motors not armed pass through throttle and exit
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if (failsafe.radio || !(ap.rc_receiver_present || motors->armed())) {
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channel_throttle->set_pwm(throttle_pwm);
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return;
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}
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// check for 3 low throttle values
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// Note: we do not pass through the low throttle until 3 low throttle values are received
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failsafe.radio_counter++;
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if( failsafe.radio_counter >= FS_COUNTER ) {
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failsafe.radio_counter = FS_COUNTER; // check to ensure we don't overflow the counter
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set_failsafe_radio(true);
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channel_throttle->set_pwm(throttle_pwm); // pass through failsafe throttle
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}
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}else{
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// we have a good throttle so reduce failsafe counter
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failsafe.radio_counter--;
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if( failsafe.radio_counter <= 0 ) {
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failsafe.radio_counter = 0; // check to ensure we don't underflow the counter
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// disengage failsafe after three (nearly) consecutive valid throttle values
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if (failsafe.radio) {
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set_failsafe_radio(false);
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}
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}
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// pass through throttle
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channel_throttle->set_pwm(throttle_pwm);
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}
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}
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#define THROTTLE_ZERO_DEBOUNCE_TIME_MS 400
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// set_throttle_zero_flag - set throttle_zero flag from debounced throttle control
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// throttle_zero is used to determine if the pilot intends to shut down the motors
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// Basically, this signals when we are not flying. We are either on the ground
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// or the pilot has shut down the copter in the air and it is free-falling
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void Copter::set_throttle_zero_flag(int16_t throttle_control)
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{
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static uint32_t last_nonzero_throttle_ms = 0;
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uint32_t tnow_ms = millis();
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// if not using throttle interlock and non-zero throttle and not E-stopped,
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// or using motor interlock and it's enabled, then motors are running,
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// and we are flying. Immediately set as non-zero
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if ((!ap.using_interlock && (throttle_control > 0) && !ap.motor_emergency_stop) ||
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(ap.using_interlock && motors->get_interlock()) ||
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ap.armed_with_switch) {
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last_nonzero_throttle_ms = tnow_ms;
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ap.throttle_zero = false;
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} else if (tnow_ms - last_nonzero_throttle_ms > THROTTLE_ZERO_DEBOUNCE_TIME_MS) {
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ap.throttle_zero = true;
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}
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}
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// pass pilot's inputs to motors library (used to allow wiggling servos while disarmed on heli, single, coax copters)
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void Copter::radio_passthrough_to_motors()
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{
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motors->set_radio_passthrough(channel_roll->norm_input(),
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channel_pitch->norm_input(),
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channel_throttle->get_control_in_zero_dz()*0.001,
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channel_yaw->norm_input());
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}
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/*
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return the throttle input for mid-stick as a control-in value
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*/
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int16_t Copter::get_throttle_mid(void)
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{
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#if TOY_MODE_ENABLED == ENABLED
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if (g2.toy_mode.enabled()) {
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return g2.toy_mode.get_throttle_mid();
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}
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#endif
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return channel_throttle->get_control_mid();
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}
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