mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-04-14 10:07:39 +08:00
- delete SubscriptionArray - all FlightTasks are now responsible for updating their own subscriptions (typically in updateInitialize()).
183 lines
6.1 KiB
C++
183 lines
6.1 KiB
C++
/****************************************************************************
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*
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* Copyright (c) 2018 PX4 Development Team. All rights reserved.
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*
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* Redistribution and use in source and binary forms, with or without
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* modification, are permitted provided that the following conditions
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* are met:
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*
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* 1. Redistributions of source code must retain the above copyright
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* notice, this list of conditions and the following disclaimer.
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* 2. Redistributions in binary form must reproduce the above copyright
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* notice, this list of conditions and the following disclaimer in
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* the documentation and/or other materials provided with the
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* distribution.
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* 3. Neither the name PX4 nor the names of its contributors may be
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* used to endorse or promote products derived from this software
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* without specific prior written permission.
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*
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* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
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* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
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* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
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* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
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* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
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* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
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* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
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* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
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* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
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* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
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* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
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* POSSIBILITY OF SUCH DAMAGE.
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*
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****************************************************************************/
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/**
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* @file FlightAutoMapper.cpp
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*/
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#include "FlightTaskAutoMapper.hpp"
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#include <mathlib/mathlib.h>
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using namespace matrix;
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bool FlightTaskAutoMapper::activate(vehicle_local_position_setpoint_s last_setpoint)
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{
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bool ret = FlightTaskAuto::activate(last_setpoint);
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_reset();
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return ret;
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}
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bool FlightTaskAutoMapper::update()
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{
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// always reset constraints because they might change depending on the type
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_setDefaultConstraints();
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_updateAltitudeAboveGround();
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bool follow_line = _type == WaypointType::loiter || _type == WaypointType::position;
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bool follow_line_prev = _type_previous == WaypointType::loiter || _type_previous == WaypointType::position;
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// 1st time that vehicle starts to follow line. Reset all setpoints to current vehicle state.
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if (follow_line && !follow_line_prev) {
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_reset();
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}
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// The only time a thrust set-point is sent out is during
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// idle. Hence, reset thrust set-point to NAN in case the
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// vehicle exits idle.
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if (_type_previous == WaypointType::idle) {
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_thrust_setpoint = Vector3f(NAN, NAN, NAN);
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}
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if (_type == WaypointType::idle) {
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_generateIdleSetpoints();
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} else if (_type == WaypointType::land) {
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_generateLandSetpoints();
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} else if (follow_line) {
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_generateSetpoints();
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} else if (_type == WaypointType::takeoff) {
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_generateTakeoffSetpoints();
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} else if (_type == WaypointType::velocity) {
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_generateVelocitySetpoints();
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}
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if (_param_com_obs_avoid.get()) {
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_obstacle_avoidance.updateAvoidanceDesiredSetpoints(_position_setpoint, _velocity_setpoint, (int)_type);
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_obstacle_avoidance.injectAvoidanceSetpoints(_position_setpoint, _velocity_setpoint, _yaw_setpoint,
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_yawspeed_setpoint);
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}
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// during mission and reposition, raise the landing gears but only
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// if altitude is high enough
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if (_highEnoughForLandingGear()) {
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_gear.landing_gear = _mission_gear;
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}
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// update previous type
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_type_previous = _type;
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return true;
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}
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void FlightTaskAutoMapper::_reset()
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{
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// Set setpoints equal current state.
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_velocity_setpoint = _velocity;
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_position_setpoint = _position;
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}
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void FlightTaskAutoMapper::_generateIdleSetpoints()
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{
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// Send zero thrust setpoint
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_position_setpoint = Vector3f(NAN, NAN, NAN); // Don't require any position/velocity setpoints
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_velocity_setpoint = Vector3f(NAN, NAN, NAN);
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_thrust_setpoint.zero();
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}
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void FlightTaskAutoMapper::_generateLandSetpoints()
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{
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// Keep xy-position and go down with landspeed
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_position_setpoint = Vector3f(_target(0), _target(1), NAN);
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_velocity_setpoint = Vector3f(Vector3f(NAN, NAN, _param_mpc_land_speed.get()));
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// set constraints
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_constraints.tilt = math::radians(_param_mpc_tiltmax_lnd.get());
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_constraints.speed_down = _param_mpc_land_speed.get();
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_gear.landing_gear = landing_gear_s::GEAR_DOWN;
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}
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void FlightTaskAutoMapper::_generateTakeoffSetpoints()
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{
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// Takeoff is completely defined by target position
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_position_setpoint = _target;
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_velocity_setpoint = Vector3f(NAN, NAN, NAN);
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// limit vertical speed during takeoff
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_constraints.speed_up = math::gradual(_alt_above_ground, _param_mpc_land_alt2.get(),
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_param_mpc_land_alt1.get(), _param_mpc_tko_speed.get(), _constraints.speed_up);
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_gear.landing_gear = landing_gear_s::GEAR_DOWN;
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}
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void FlightTaskAutoMapper::_generateVelocitySetpoints()
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{
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// TODO: Remove velocity force logic from navigator, since
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// navigator should only send out waypoints.
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_position_setpoint = Vector3f(NAN, NAN, _position(2));
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Vector2f vel_sp_xy = Vector2f(_velocity).unit_or_zero() * _mc_cruise_speed;
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_velocity_setpoint = Vector3f(vel_sp_xy(0), vel_sp_xy(1), NAN);
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}
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void FlightTaskAutoMapper::_updateAltitudeAboveGround()
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{
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// Altitude above ground is by default just the negation of the current local position in D-direction.
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_alt_above_ground = -_position(2);
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if (PX4_ISFINITE(_dist_to_bottom)) {
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// We have a valid distance to ground measurement
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_alt_above_ground = _dist_to_bottom;
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} else if (_sub_home_position.get().valid_alt) {
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// if home position is set, then altitude above ground is relative to the home position
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_alt_above_ground = -_position(2) + _sub_home_position.get().z;
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}
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}
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void FlightTaskAutoMapper::updateParams()
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{
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FlightTaskAuto::updateParams();
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// make sure that alt1 is above alt2
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_param_mpc_land_alt1.set(math::max(_param_mpc_land_alt1.get(), _param_mpc_land_alt2.get()));
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}
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bool FlightTaskAutoMapper::_highEnoughForLandingGear()
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{
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// return true if altitude is above two meters
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return _alt_above_ground > 2.0f;
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}
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