ardupilot/ArduCopter/takeoff.cpp

231 lines
7.8 KiB
C++
Raw Normal View History

#include "Copter.h"
Mode::_TakeOff Mode::takeoff;
2019-11-28 09:19:17 -04:00
bool Mode::auto_takeoff_no_nav_active = false;
float Mode::auto_takeoff_no_nav_alt_cm = 0;
2015-04-29 23:52:19 -03:00
// This file contains the high-level takeoff logic for Loiter, PosHold, AltHold, Sport modes.
// The take-off can be initiated from a GCS NAV_TAKEOFF command which includes a takeoff altitude
// A safe takeoff speed is calculated and used to calculate a time_ms
// the pos_control target is then slowly increased until time_ms expires
bool Mode::do_user_takeoff_start(float takeoff_alt_cm)
2017-12-12 06:09:48 -04:00
{
copter.flightmode->takeoff.start(takeoff_alt_cm);
2017-12-12 06:09:48 -04:00
return true;
}
2015-04-29 23:52:19 -03:00
// initiate user takeoff - called when MAVLink TAKEOFF command is received
bool Mode::do_user_takeoff(float takeoff_alt_cm, bool must_navigate)
{
2017-12-12 06:09:48 -04:00
if (!copter.motors->armed()) {
return false;
}
if (!copter.ap.land_complete) {
2017-12-12 06:09:48 -04:00
// can't takeoff again!
return false;
}
if (!has_user_takeoff(must_navigate)) {
// this mode doesn't support user takeoff
return false;
}
if (takeoff_alt_cm <= copter.current_loc.alt) {
// can't takeoff downwards...
return false;
}
2017-12-12 06:09:48 -04:00
// Helicopters should return false if MAVlink takeoff command is received while the rotor is not spinning
if (motors->get_spool_state() != AP_Motors::SpoolState::THROTTLE_UNLIMITED && copter.ap.using_interlock) {
2017-12-12 06:09:48 -04:00
return false;
}
2017-12-12 06:09:48 -04:00
if (!do_user_takeoff_start(takeoff_alt_cm)) {
return false;
}
2017-12-12 06:09:48 -04:00
copter.set_auto_armed(true);
return true;
}
// start takeoff to specified altitude above home in centimeters
void Mode::_TakeOff::start(float alt_cm)
{
// indicate we are taking off
copter.set_land_complete(false);
// tell position controller to reset alt target and reset I terms
copter.flightmode->set_throttle_takeoff();
2015-04-29 23:52:19 -03:00
// calculate climb rate
const float speed = MIN(copter.wp_nav->get_default_speed_up(), MAX(copter.g.pilot_speed_up*2.0f/3.0f, copter.g.pilot_speed_up-50.0f));
2015-04-29 23:52:19 -03:00
// sanity check speed and target
if (speed <= 0.0f || alt_cm <= 0.0f) {
return;
}
2015-04-29 23:52:19 -03:00
// initialise takeoff state
_running = true;
max_speed = speed;
start_ms = millis();
alt_delta = alt_cm;
}
2015-04-30 03:52:32 -03:00
// stop takeoff
void Mode::_TakeOff::stop()
2015-04-30 03:52:32 -03:00
{
_running = false;
start_ms = 0;
2015-04-30 03:52:32 -03:00
}
// returns pilot and takeoff climb rates
// pilot_climb_rate is both an input and an output
// takeoff_climb_rate is only an output
// has side-effect of turning takeoff off when timeout as expired
void Mode::_TakeOff::get_climb_rates(float& pilot_climb_rate,
float& takeoff_climb_rate)
{
// return pilot_climb_rate if take-off inactive
if (!_running) {
takeoff_climb_rate = 0.0f;
return;
}
// acceleration of 50cm/s/s
static constexpr float TAKEOFF_ACCEL = 50.0f;
const float takeoff_minspeed = MIN(50.0f, max_speed);
const float time_elapsed = (millis() - start_ms) * 1.0e-3f;
const float speed = MIN(time_elapsed * TAKEOFF_ACCEL + takeoff_minspeed, max_speed);
2015-10-19 21:56:49 -03:00
const float time_to_max_speed = (max_speed - takeoff_minspeed) / TAKEOFF_ACCEL;
2015-10-19 21:56:49 -03:00
float height_gained;
if (time_elapsed <= time_to_max_speed) {
height_gained = 0.5f * TAKEOFF_ACCEL * sq(time_elapsed) + takeoff_minspeed * time_elapsed;
2015-10-19 21:56:49 -03:00
} else {
height_gained = 0.5f * TAKEOFF_ACCEL * sq(time_to_max_speed) + takeoff_minspeed * time_to_max_speed +
(time_elapsed - time_to_max_speed) * max_speed;
2015-10-19 21:56:49 -03:00
}
// check if the takeoff is over
if (height_gained >= alt_delta) {
stop();
}
// if takeoff climb rate is zero return
2015-10-19 21:56:49 -03:00
if (speed <= 0.0f) {
takeoff_climb_rate = 0.0f;
return;
}
// default take-off climb rate to maximum speed
2015-10-19 21:56:49 -03:00
takeoff_climb_rate = speed;
// if pilot's commands descent
if (pilot_climb_rate < 0.0f) {
// if overall climb rate is still positive, move to take-off climb rate
if (takeoff_climb_rate + pilot_climb_rate > 0.0f) {
takeoff_climb_rate = takeoff_climb_rate + pilot_climb_rate;
pilot_climb_rate = 0.0f;
} else {
// if overall is negative, move to pilot climb rate
pilot_climb_rate = pilot_climb_rate + takeoff_climb_rate;
takeoff_climb_rate = 0.0f;
}
} else { // pilot commands climb
// pilot climb rate is zero until it surpasses the take-off climb rate
if (pilot_climb_rate > takeoff_climb_rate) {
pilot_climb_rate = pilot_climb_rate - takeoff_climb_rate;
} else {
pilot_climb_rate = 0.0f;
}
}
}
void Mode::auto_takeoff_run()
{
// if not armed set throttle to zero and exit immediately
if (!motors->armed() || !copter.ap.auto_armed) {
make_safe_spool_down();
wp_nav->shift_wp_origin_to_current_pos();
return;
}
2019-11-28 09:19:17 -04:00
// set motors to full range
motors->set_desired_spool_state(AP_Motors::DesiredSpoolState::THROTTLE_UNLIMITED);
// process pilot's yaw input
float target_yaw_rate = 0;
if (!copter.failsafe.radio) {
// get pilot's desired yaw rate
target_yaw_rate = get_pilot_desired_yaw_rate(channel_yaw->get_control_in());
}
// aircraft stays in landed state until rotor speed runup has finished
if (motors->get_spool_state() == AP_Motors::SpoolState::THROTTLE_UNLIMITED) {
set_land_complete(false);
} else {
// motors have not completed spool up yet so relax navigation and position controllers
wp_nav->shift_wp_origin_to_current_pos();
pos_control->relax_alt_hold_controllers(0.0f); // forces throttle output to go to zero
pos_control->update_z_controller();
attitude_control->set_yaw_target_to_current_heading();
attitude_control->reset_rate_controller_I_terms();
attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(0.0f, 0.0f, 0.0f);
return;
}
2019-11-28 09:19:17 -04:00
// check if we are not navigating because of low altitude
float nav_roll = 0.0f, nav_pitch = 0.0f;
if (auto_takeoff_no_nav_active) {
// check if vehicle has reached no_nav_alt threshold
if (inertial_nav.get_altitude() >= auto_takeoff_no_nav_alt_cm) {
auto_takeoff_no_nav_active = false;
wp_nav->shift_wp_origin_and_destination_to_stopping_point_xy();
} else {
// shift the navigation target horizontally to our current position
wp_nav->shift_wp_origin_and_destination_to_current_pos_xy();
}
// tell the position controller that we have limited roll/pitch demand to prevent integrator buildup
pos_control->set_limit_accel_xy();
}
// run waypoint controller
copter.failsafe_terrain_set_status(wp_nav->update_wpnav());
2019-11-28 09:19:17 -04:00
if (!auto_takeoff_no_nav_active) {
nav_roll = wp_nav->get_roll();
nav_pitch = wp_nav->get_pitch();
}
// call z-axis position controller (wpnav should have already updated it's alt target)
copter.pos_control->update_z_controller();
2019-11-28 09:19:17 -04:00
// roll & pitch from waypoint controller, yaw rate from pilot
attitude_control->input_euler_angle_roll_pitch_euler_rate_yaw(nav_roll, nav_pitch, target_yaw_rate);
}
void Mode::auto_takeoff_set_start_alt(void)
{
2019-11-28 09:19:17 -04:00
if ((g2.wp_navalt_min > 0) && (is_disarmed_or_landed() || !motors->get_interlock())) {
// we are not flying, climb with no navigation to current alt-above-ekf-origin + wp_navalt_min
auto_takeoff_no_nav_alt_cm = inertial_nav.get_altitude() + g2.wp_navalt_min * 100;
auto_takeoff_no_nav_active = true;
} else {
2019-11-28 09:19:17 -04:00
auto_takeoff_no_nav_active = false;
}
}
bool Mode::is_taking_off() const
{
if (!has_user_takeoff(false)) {
return false;
}
if (copter.ap.land_complete) {
return false;
}
if (takeoff.running()) {
return true;
}
return false;
}