mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-04-14 10:07:39 +08:00
180 lines
6.3 KiB
C++
180 lines
6.3 KiB
C++
/****************************************************************************
|
|
*
|
|
* Copyright (c) 2018 PX4 Development Team. All rights reserved.
|
|
*
|
|
* Redistribution and use in source and binary forms, with or without
|
|
* modification, are permitted provided that the following conditions
|
|
* are met:
|
|
*
|
|
* 1. Redistributions of source code must retain the above copyright
|
|
* notice, this list of conditions and the following disclaimer.
|
|
* 2. Redistributions in binary form must reproduce the above copyright
|
|
* notice, this list of conditions and the following disclaimer in
|
|
* the documentation and/or other materials provided with the
|
|
* distribution.
|
|
* 3. Neither the name PX4 nor the names of its contributors may be
|
|
* used to endorse or promote products derived from this software
|
|
* without specific prior written permission.
|
|
*
|
|
* THIS SOFTWARE IS PROVIDED BY THE COPYRIGHT HOLDERS AND CONTRIBUTORS
|
|
* "AS IS" AND ANY EXPRESS OR IMPLIED WARRANTIES, INCLUDING, BUT NOT
|
|
* LIMITED TO, THE IMPLIED WARRANTIES OF MERCHANTABILITY AND FITNESS
|
|
* FOR A PARTICULAR PURPOSE ARE DISCLAIMED. IN NO EVENT SHALL THE
|
|
* COPYRIGHT OWNER OR CONTRIBUTORS BE LIABLE FOR ANY DIRECT, INDIRECT,
|
|
* INCIDENTAL, SPECIAL, EXEMPLARY, OR CONSEQUENTIAL DAMAGES (INCLUDING,
|
|
* BUT NOT LIMITED TO, PROCUREMENT OF SUBSTITUTE GOODS OR SERVICES; LOSS
|
|
* OF USE, DATA, OR PROFITS; OR BUSINESS INTERRUPTION) HOWEVER CAUSED
|
|
* AND ON ANY THEORY OF LIABILITY, WHETHER IN CONTRACT, STRICT
|
|
* LIABILITY, OR TORT (INCLUDING NEGLIGENCE OR OTHERWISE) ARISING IN
|
|
* ANY WAY OUT OF THE USE OF THIS SOFTWARE, EVEN IF ADVISED OF THE
|
|
* POSSIBILITY OF SUCH DAMAGE.
|
|
*
|
|
****************************************************************************/
|
|
|
|
/**
|
|
* @file FlightTaskManualPosition.cpp
|
|
*/
|
|
|
|
#include "FlightTaskManualPosition.hpp"
|
|
#include <mathlib/mathlib.h>
|
|
#include <float.h>
|
|
|
|
using namespace matrix;
|
|
|
|
FlightTaskManualPosition::FlightTaskManualPosition() : _collision_prevention(this)
|
|
{
|
|
|
|
}
|
|
|
|
bool FlightTaskManualPosition::updateInitialize()
|
|
{
|
|
bool ret = FlightTaskManualAltitude::updateInitialize();
|
|
// require valid position / velocity in xy
|
|
return ret && PX4_ISFINITE(_position(0))
|
|
&& PX4_ISFINITE(_position(1))
|
|
&& PX4_ISFINITE(_velocity(0))
|
|
&& PX4_ISFINITE(_velocity(1));
|
|
}
|
|
|
|
bool FlightTaskManualPosition::activate(const vehicle_local_position_setpoint_s &last_setpoint)
|
|
{
|
|
// all requirements from altitude-mode still have to hold
|
|
bool ret = FlightTaskManualAltitude::activate(last_setpoint);
|
|
|
|
// set task specific constraint
|
|
if (_constraints.speed_xy >= _param_mpc_vel_manual.get()) {
|
|
_constraints.speed_xy = _param_mpc_vel_manual.get();
|
|
}
|
|
|
|
_position_setpoint(0) = _position(0);
|
|
_position_setpoint(1) = _position(1);
|
|
_velocity_setpoint(0) = _velocity_setpoint(1) = 0.0f;
|
|
_velocity_scale = _constraints.speed_xy;
|
|
|
|
// for position-controlled mode, we need a valid position and velocity state
|
|
// in NE-direction
|
|
return ret;
|
|
}
|
|
|
|
void FlightTaskManualPosition::_scaleSticks()
|
|
{
|
|
/* Use same scaling as for FlightTaskManualAltitude */
|
|
FlightTaskManualAltitude::_scaleSticks();
|
|
|
|
/* Constrain length of stick inputs to 1 for xy*/
|
|
Vector2f stick_xy = _sticks.getPositionExpo().slice<2, 1>(0, 0);
|
|
|
|
const float mag = math::constrain(stick_xy.length(), 0.0f, 1.0f);
|
|
|
|
if (mag > FLT_EPSILON) {
|
|
stick_xy = stick_xy.normalized() * mag;
|
|
}
|
|
|
|
const float max_speed_from_estimator = _sub_vehicle_local_position.get().vxy_max;
|
|
|
|
if (PX4_ISFINITE(max_speed_from_estimator)) {
|
|
// use the minimum of the estimator and user specified limit
|
|
_velocity_scale = fminf(_constraints.speed_xy, max_speed_from_estimator);
|
|
// Allow for a minimum of 0.3 m/s for repositioning
|
|
_velocity_scale = fmaxf(_velocity_scale, 0.3f);
|
|
|
|
} else {
|
|
_velocity_scale = _constraints.speed_xy;
|
|
}
|
|
|
|
_velocity_scale = fminf(_computeVelXYGroundDist(), _velocity_scale);
|
|
|
|
// scale velocity to its maximum limits
|
|
Vector2f vel_sp_xy = stick_xy * _velocity_scale;
|
|
|
|
/* Rotate setpoint into local frame. */
|
|
_rotateIntoHeadingFrame(vel_sp_xy);
|
|
|
|
// collision prevention
|
|
if (_collision_prevention.is_active()) {
|
|
_collision_prevention.modifySetpoint(vel_sp_xy, _velocity_scale, _position.xy(), _velocity.xy());
|
|
}
|
|
|
|
_velocity_setpoint.xy() = vel_sp_xy;
|
|
}
|
|
|
|
float FlightTaskManualPosition::_computeVelXYGroundDist()
|
|
{
|
|
float max_vel_xy = _constraints.speed_xy;
|
|
|
|
// limit speed gradually within the altitudes MPC_LAND_ALT1 and MPC_LAND_ALT2
|
|
if (PX4_ISFINITE(_dist_to_ground)) {
|
|
max_vel_xy = math::gradual(_dist_to_ground,
|
|
_param_mpc_land_alt2.get(), _param_mpc_land_alt1.get(),
|
|
_param_mpc_land_vel_xy.get(), _constraints.speed_xy);
|
|
}
|
|
|
|
return max_vel_xy;
|
|
}
|
|
|
|
void FlightTaskManualPosition::_updateXYlock()
|
|
{
|
|
/* If position lock is not active, position setpoint is set to NAN.*/
|
|
const float vel_xy_norm = Vector2f(_velocity).length();
|
|
const bool apply_brake = Vector2f(_velocity_setpoint).length() < FLT_EPSILON;
|
|
const bool stopped = (_param_mpc_hold_max_xy.get() < FLT_EPSILON || vel_xy_norm < _param_mpc_hold_max_xy.get());
|
|
|
|
if (apply_brake && stopped && !PX4_ISFINITE(_position_setpoint(0))) {
|
|
_position_setpoint(0) = _position(0);
|
|
_position_setpoint(1) = _position(1);
|
|
|
|
} else if (PX4_ISFINITE(_position_setpoint(0)) && apply_brake) {
|
|
// Position is locked but check if a reset event has happened.
|
|
// We will shift the setpoints.
|
|
if (_sub_vehicle_local_position.get().xy_reset_counter != _reset_counter) {
|
|
_position_setpoint(0) = _position(0);
|
|
_position_setpoint(1) = _position(1);
|
|
_reset_counter = _sub_vehicle_local_position.get().xy_reset_counter;
|
|
}
|
|
|
|
} else {
|
|
/* don't lock*/
|
|
_position_setpoint(0) = NAN;
|
|
_position_setpoint(1) = NAN;
|
|
}
|
|
}
|
|
|
|
void FlightTaskManualPosition::_updateSetpoints()
|
|
{
|
|
FlightTaskManualAltitude::_updateSetpoints(); // needed to get yaw and setpoints in z-direction
|
|
_acceleration_setpoint.setNaN(); // don't use the horizontal setpoints from FlightTaskAltitude
|
|
|
|
_updateXYlock(); // check for position lock
|
|
|
|
// check if an external yaw handler is active and if yes, let it update the yaw setpoints
|
|
if (_weathervane_yaw_handler != nullptr && _weathervane_yaw_handler->is_active()) {
|
|
_yaw_setpoint = NAN;
|
|
|
|
// only enable the weathervane to change the yawrate when position lock is active (and thus the pos. sp. are NAN)
|
|
if (PX4_ISFINITE(_position_setpoint(0)) && PX4_ISFINITE(_position_setpoint(1))) {
|
|
// vehicle is steady
|
|
_yawspeed_setpoint += _weathervane_yaw_handler->get_weathervane_yawrate();
|
|
}
|
|
}
|
|
}
|