2018-10-23 14:06:40 +02:00
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/****************************************************************************
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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 FlightAutoLine.cpp
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*/
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#include "FlightTaskAutoLineSmoothVel.hpp"
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#include <mathlib/mathlib.h>
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#include <float.h>
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2019-07-30 15:15:22 +02:00
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#include "TrajMath.hpp"
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2018-10-23 14:06:40 +02:00
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using namespace matrix;
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2019-07-15 17:57:40 +02:00
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bool FlightTaskAutoLineSmoothVel::activate(vehicle_local_position_setpoint_s last_setpoint)
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2018-10-23 14:06:40 +02:00
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{
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2019-07-15 17:57:40 +02:00
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bool ret = FlightTaskAutoMapper2::activate(last_setpoint);
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2019-07-02 16:11:44 +02:00
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2019-07-15 17:57:40 +02:00
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checkSetpoints(last_setpoint);
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const Vector3f accel_prev(last_setpoint.acc_x, last_setpoint.acc_y, last_setpoint.acc_z);
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const Vector3f vel_prev(last_setpoint.vx, last_setpoint.vy, last_setpoint.vz);
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const Vector3f pos_prev(last_setpoint.x, last_setpoint.y, last_setpoint.z);
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2018-10-23 14:06:40 +02:00
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for (int i = 0; i < 3; ++i) {
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2019-07-02 16:11:44 +02:00
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_trajectory[i].reset(accel_prev(i), vel_prev(i), pos_prev(i));
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2018-10-23 14:06:40 +02:00
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}
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2019-07-15 17:57:40 +02:00
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_yaw_sp_prev = last_setpoint.yaw;
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2018-10-25 15:29:45 +02:00
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_updateTrajConstraints();
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2019-07-02 16:39:48 +02:00
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_initEkfResetCounters();
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2018-10-25 15:29:45 +02:00
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2018-10-23 14:06:40 +02:00
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return ret;
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}
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2018-10-23 15:24:57 +02:00
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void FlightTaskAutoLineSmoothVel::reActivate()
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{
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2019-05-14 11:07:34 +02:00
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// On ground, reset acceleration and velocity to zero
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for (int i = 0; i < 2; ++i) {
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_trajectory[i].reset(0.f, 0.f, _position(i));
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}
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_trajectory[2].reset(0.f, 0.7f, _position(2));
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2019-07-02 16:39:48 +02:00
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_initEkfResetCounters();
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2018-10-23 15:24:57 +02:00
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}
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2019-07-08 10:57:50 +02:00
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void FlightTaskAutoLineSmoothVel::checkSetpoints(vehicle_local_position_setpoint_s &setpoints)
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{
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// If the position setpoint is unknown, set to the current postion
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if (!PX4_ISFINITE(setpoints.x)) { setpoints.x = _position(0); }
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if (!PX4_ISFINITE(setpoints.y)) { setpoints.y = _position(1); }
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if (!PX4_ISFINITE(setpoints.z)) { setpoints.z = _position(2); }
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// If the velocity setpoint is unknown, set to the current velocity
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if (!PX4_ISFINITE(setpoints.vx)) { setpoints.vx = _velocity(0); }
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if (!PX4_ISFINITE(setpoints.vy)) { setpoints.vy = _velocity(1); }
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if (!PX4_ISFINITE(setpoints.vz)) { setpoints.vz = _velocity(2); }
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// No acceleration estimate available, set to zero if the setpoint is NAN
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if (!PX4_ISFINITE(setpoints.acc_x)) { setpoints.acc_x = 0.f; }
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if (!PX4_ISFINITE(setpoints.acc_y)) { setpoints.acc_y = 0.f; }
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if (!PX4_ISFINITE(setpoints.acc_z)) { setpoints.acc_z = 0.f; }
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if (!PX4_ISFINITE(setpoints.yaw)) { setpoints.yaw = _yaw; }
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}
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2018-10-23 14:06:40 +02:00
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void FlightTaskAutoLineSmoothVel::_generateSetpoints()
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{
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2018-10-26 11:24:10 +02:00
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_prepareSetpoints();
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_generateTrajectory();
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2019-02-21 16:28:33 +01:00
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if (!PX4_ISFINITE(_yaw_setpoint) && !PX4_ISFINITE(_yawspeed_setpoint)) {
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2018-10-26 11:24:10 +02:00
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// no valid heading -> generate heading in this flight task
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_generateHeading();
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2018-10-23 14:06:40 +02:00
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}
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2018-10-26 11:24:10 +02:00
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}
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2018-10-23 14:06:40 +02:00
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2018-10-26 11:24:10 +02:00
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void FlightTaskAutoLineSmoothVel::_generateHeading()
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{
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// Generate heading along trajectory if possible, otherwise hold the previous yaw setpoint
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if (!_generateHeadingAlongTraj()) {
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_yaw_setpoint = _yaw_sp_prev;
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}
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2018-10-23 14:06:40 +02:00
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}
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2018-10-26 11:24:10 +02:00
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bool FlightTaskAutoLineSmoothVel::_generateHeadingAlongTraj()
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2018-10-23 14:06:40 +02:00
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{
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2018-10-26 11:24:10 +02:00
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bool res = false;
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Vector2f vel_sp_xy(_velocity_setpoint);
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2019-08-05 13:28:14 +02:00
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Vector2f traj_to_target = Vector2f(_target) - Vector2f(_position);
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2018-10-26 11:24:10 +02:00
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2019-08-05 13:28:14 +02:00
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if ((vel_sp_xy.length() > .1f) &&
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(traj_to_target.length() > _target_acceptance_radius)) {
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2018-10-26 11:24:10 +02:00
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// Generate heading from velocity vector, only if it is long enough
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2019-08-05 13:28:14 +02:00
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// and if the drone is far enough from the target
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2018-10-26 11:24:10 +02:00
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_compute_heading_from_2D_vector(_yaw_setpoint, vel_sp_xy);
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res = true;
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}
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2018-10-23 14:06:40 +02:00
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2018-10-26 11:24:10 +02:00
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return res;
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2018-10-23 14:06:40 +02:00
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}
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/* Constrain some value vith a constrain depending on the sign of the constrain
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* Example: - if the constrain is -5, the value will be constrained between -5 and 0
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* - if the constrain is 5, the value will be constrained between 0 and 5
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*/
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2019-03-13 11:19:23 +01:00
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inline float FlightTaskAutoLineSmoothVel::_constrainOneSide(float val, float constrain)
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2018-10-23 14:06:40 +02:00
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{
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const float min = (constrain < FLT_EPSILON) ? constrain : 0.f;
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const float max = (constrain > FLT_EPSILON) ? constrain : 0.f;
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return math::constrain(val, min, max);
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}
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2019-07-02 16:39:48 +02:00
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void FlightTaskAutoLineSmoothVel::_initEkfResetCounters()
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{
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_reset_counters.xy = _sub_vehicle_local_position->get().xy_reset_counter;
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_reset_counters.vxy = _sub_vehicle_local_position->get().vxy_reset_counter;
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_reset_counters.z = _sub_vehicle_local_position->get().z_reset_counter;
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_reset_counters.vz = _sub_vehicle_local_position->get().vz_reset_counter;
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}
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2019-03-13 11:24:06 +01:00
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void FlightTaskAutoLineSmoothVel::_checkEkfResetCounters()
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{
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// Check if a reset event has happened.
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if (_sub_vehicle_local_position->get().xy_reset_counter != _reset_counters.xy) {
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_trajectory[0].setCurrentPosition(_position(0));
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_trajectory[1].setCurrentPosition(_position(1));
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_reset_counters.xy = _sub_vehicle_local_position->get().xy_reset_counter;
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}
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if (_sub_vehicle_local_position->get().vxy_reset_counter != _reset_counters.vxy) {
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_trajectory[0].setCurrentVelocity(_velocity(0));
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_trajectory[1].setCurrentVelocity(_velocity(1));
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_reset_counters.vxy = _sub_vehicle_local_position->get().vxy_reset_counter;
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}
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if (_sub_vehicle_local_position->get().z_reset_counter != _reset_counters.z) {
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_trajectory[2].setCurrentPosition(_position(2));
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_reset_counters.z = _sub_vehicle_local_position->get().z_reset_counter;
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}
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if (_sub_vehicle_local_position->get().vz_reset_counter != _reset_counters.vz) {
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_trajectory[2].setCurrentVelocity(_velocity(2));
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_reset_counters.vz = _sub_vehicle_local_position->get().vz_reset_counter;
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}
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}
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2019-07-16 15:34:48 +02:00
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float FlightTaskAutoLineSmoothVel::_getSpeedAtTarget()
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{
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2019-07-30 15:15:22 +02:00
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// Compute the maximum allowed speed at the waypoint assuming that we want to
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// connect the two lines (prev-current and current-next)
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2019-07-16 15:34:48 +02:00
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// with a tangent circle with constant speed and desired centripetal acceleration: a_centripetal = speed^2 / radius
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2019-07-30 15:15:22 +02:00
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// The circle should in theory start and end at the intersection of the lines and the waypoint's acceptance radius.
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// This is not exactly true in reality since Navigator switches the waypoint so we have to take in account that
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// the real acceptance radius is smaller.
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// It can be that the next waypoint is the last one or that the drone will have to stop for some other reason
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// so we have to make sure that the speed at the current waypoint allows to stop at the next waypoint.
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2019-07-16 15:34:48 +02:00
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float speed_at_target = 0.0f;
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const float distance_current_next = Vector2f(&(_target - _next_wp)(0)).length();
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2019-07-19 14:31:19 +02:00
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const bool waypoint_overlap = Vector2f(&(_target - _prev_wp)(0)).length() < _target_acceptance_radius;
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const bool yaw_align_check_pass = (_param_mpc_yaw_mode.get() != 4) || _yaw_sp_aligned;
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2019-07-16 15:34:48 +02:00
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if (distance_current_next > 0.001f &&
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2019-07-19 14:31:19 +02:00
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!waypoint_overlap &&
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yaw_align_check_pass) {
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2019-07-16 15:34:48 +02:00
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// Max speed between current and next
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const float max_speed_current_next = _getMaxSpeedFromDistance(distance_current_next);
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2019-07-19 14:37:03 +02:00
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const float alpha = acos(Vector2f(&(_target - _prev_wp)(0)).unit_or_zero() *
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2019-07-30 15:15:22 +02:00
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Vector2f(&(_target - _next_wp)(0)).unit_or_zero());
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// We choose a maximum centripetal acceleration of MPC_ACC_HOR * MPC_XY_TRAJ_P to take in account
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// that there is a jerk limit (a direct transition from line to circle is not possible)
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2019-07-19 14:37:03 +02:00
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// MPC_XY_TRAJ_P should be between 0 and 1.
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2019-07-30 15:15:22 +02:00
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const float max_speed_in_turn = trajmath::computeMaxSpeedInWaypoint(alpha,
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_param_mpc_xy_traj_p.get() * _param_mpc_acc_hor.get(),
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_target_acceptance_radius);
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2019-07-19 14:37:03 +02:00
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speed_at_target = math::min(math::min(max_speed_in_turn, max_speed_current_next), _mc_cruise_speed);
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2019-07-16 15:34:48 +02:00
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}
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return speed_at_target;
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}
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float FlightTaskAutoLineSmoothVel::_getMaxSpeedFromDistance(float braking_distance)
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{
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2019-07-30 15:15:22 +02:00
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float max_speed = trajmath::computeMaxSpeedFromBrakingDistance(_param_mpc_jerk_auto.get(),
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_param_mpc_acc_hor.get(),
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braking_distance);
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// To avoid high gain at low distance due to the sqrt, we take the minimum
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// of this velocity and a slope of "traj_p" m/s per meter
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2019-07-16 15:34:48 +02:00
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max_speed = math::min(max_speed, braking_distance * _param_mpc_xy_traj_p.get());
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return max_speed;
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}
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2018-10-23 14:06:40 +02:00
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void FlightTaskAutoLineSmoothVel::_prepareSetpoints()
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{
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// Interface: A valid position setpoint generates a velocity target using a P controller. If a velocity is specified
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// that one is used as a velocity limit.
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// If the position setpoints are set to NAN, the values in the velocity setpoints are used as velocity targets: nothing to do here.
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2019-03-13 11:24:06 +01:00
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_checkEkfResetCounters();
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2019-05-14 11:07:34 +02:00
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_want_takeoff = false;
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2018-12-13 17:45:14 +01:00
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2019-06-27 14:07:48 +02:00
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if (_param_mpc_yaw_mode.get() == 4 && !_yaw_sp_aligned) {
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// Wait for the yaw setpoint to be aligned
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_velocity_setpoint.setAll(0.f);
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} else {
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if (PX4_ISFINITE(_position_setpoint(0)) &&
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PX4_ISFINITE(_position_setpoint(1))) {
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// Use position setpoints to generate velocity setpoints
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// Get various path specific vectors. */
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2019-07-18 13:53:39 +02:00
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Vector3f pos_traj;
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2019-06-27 14:07:48 +02:00
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pos_traj(0) = _trajectory[0].getCurrentPosition();
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pos_traj(1) = _trajectory[1].getCurrentPosition();
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2019-07-18 13:53:39 +02:00
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pos_traj(2) = _trajectory[2].getCurrentPosition();
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Vector2f pos_traj_to_dest_xy(_position_setpoint - pos_traj);
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Vector2f u_pos_traj_to_dest_xy(pos_traj_to_dest_xy.unit_or_zero());
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const bool has_reached_altitude = fabsf(_position_setpoint(2) - pos_traj(2)) < _param_nav_mc_alt_rad.get();
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2019-06-27 14:07:48 +02:00
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2019-07-18 13:53:39 +02:00
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float speed_sp_track = _getMaxSpeedFromDistance(pos_traj_to_dest_xy.length());
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2019-07-16 15:34:48 +02:00
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2019-07-18 13:53:39 +02:00
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|
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if (has_reached_altitude) {
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speed_sp_track = math::constrain(speed_sp_track, _getSpeedAtTarget(), _mc_cruise_speed);
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} else {
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speed_sp_track = math::constrain(speed_sp_track, 0.0f, _mc_cruise_speed);
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}
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2019-06-27 14:07:48 +02:00
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Vector2f vel_sp_xy = u_pos_traj_to_dest_xy * speed_sp_track;
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for (int i = 0; i < 2; i++) {
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// If available, constrain the velocity using _velocity_setpoint(.)
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if (PX4_ISFINITE(_velocity_setpoint(i))) {
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_velocity_setpoint(i) = _constrainOneSide(vel_sp_xy(i), _velocity_setpoint(i));
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} else {
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_velocity_setpoint(i) = vel_sp_xy(i);
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}
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2018-10-23 14:06:40 +02:00
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}
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}
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2019-06-27 14:07:48 +02:00
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if (PX4_ISFINITE(_position_setpoint(2))) {
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const float vel_sp_z = (_position_setpoint(2) - _trajectory[2].getCurrentPosition()) *
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_param_mpc_z_traj_p.get(); // Generate a velocity target for the trajectory using a simple P loop
|
2018-10-23 14:06:40 +02:00
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|
2019-06-27 14:07:48 +02:00
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|
// If available, constrain the velocity using _velocity_setpoint(.)
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|
if (PX4_ISFINITE(_velocity_setpoint(2))) {
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_velocity_setpoint(2) = _constrainOneSide(vel_sp_z, _velocity_setpoint(2));
|
2018-10-23 14:06:40 +02:00
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|
2019-06-27 14:07:48 +02:00
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} else {
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|
_velocity_setpoint(2) = vel_sp_z;
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}
|
2018-10-23 14:06:40 +02:00
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|
2019-06-27 14:07:48 +02:00
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_want_takeoff = _velocity_setpoint(2) < -0.3f;
|
2018-10-23 14:06:40 +02:00
|
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|
}
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}
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}
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|
2018-10-25 15:29:45 +02:00
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|
|
void FlightTaskAutoLineSmoothVel::_updateTrajConstraints()
|
2018-10-23 14:06:40 +02:00
|
|
|
{
|
|
|
|
|
// Update the constraints of the trajectories
|
2019-06-13 10:19:15 +02:00
|
|
|
_trajectory[0].setMaxAccel(_param_mpc_acc_hor.get()); // TODO : Should be computed using heading
|
|
|
|
|
_trajectory[1].setMaxAccel(_param_mpc_acc_hor.get());
|
2019-04-15 12:07:20 +02:00
|
|
|
_trajectory[0].setMaxVel(_param_mpc_xy_vel_max.get());
|
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|
_trajectory[1].setMaxVel(_param_mpc_xy_vel_max.get());
|
2019-05-14 08:49:39 +02:00
|
|
|
_trajectory[0].setMaxJerk(_param_mpc_jerk_auto.get()); // TODO : Should be computed using heading
|
|
|
|
|
_trajectory[1].setMaxJerk(_param_mpc_jerk_auto.get());
|
|
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|
|
_trajectory[2].setMaxJerk(_param_mpc_jerk_auto.get());
|
2018-10-23 14:06:40 +02:00
|
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|
|
|
|
|
if (_velocity_setpoint(2) < 0.f) { // up
|
2019-03-20 10:28:17 +01:00
|
|
|
_trajectory[2].setMaxAccel(_param_mpc_acc_up_max.get());
|
|
|
|
|
_trajectory[2].setMaxVel(_param_mpc_z_vel_max_up.get());
|
2018-10-23 14:06:40 +02:00
|
|
|
|
|
|
|
|
} else { // down
|
2019-03-20 10:28:17 +01:00
|
|
|
_trajectory[2].setMaxAccel(_param_mpc_acc_down_max.get());
|
|
|
|
|
_trajectory[2].setMaxVel(_param_mpc_z_vel_max_dn.get());
|
2018-10-23 14:06:40 +02:00
|
|
|
}
|
2018-10-25 15:29:45 +02:00
|
|
|
}
|
2018-10-23 14:06:40 +02:00
|
|
|
|
2018-10-25 15:29:45 +02:00
|
|
|
void FlightTaskAutoLineSmoothVel::_generateTrajectory()
|
|
|
|
|
{
|
2019-01-17 13:59:08 +01:00
|
|
|
if (!PX4_ISFINITE(_velocity_setpoint(0)) || !PX4_ISFINITE(_velocity_setpoint(1))
|
|
|
|
|
|| !PX4_ISFINITE(_velocity_setpoint(2))) {
|
|
|
|
|
return;
|
|
|
|
|
}
|
|
|
|
|
|
2018-10-23 14:06:40 +02:00
|
|
|
/* Slow down the trajectory by decreasing the integration time based on the position error.
|
|
|
|
|
* This is only performed when the drone is behind the trajectory
|
|
|
|
|
*/
|
|
|
|
|
Vector2f position_trajectory_xy(_trajectory[0].getCurrentPosition(), _trajectory[1].getCurrentPosition());
|
|
|
|
|
Vector2f position_xy(_position);
|
|
|
|
|
Vector2f vel_traj_xy(_trajectory[0].getCurrentVelocity(), _trajectory[1].getCurrentVelocity());
|
|
|
|
|
Vector2f drone_to_trajectory_xy(position_trajectory_xy - position_xy);
|
|
|
|
|
float position_error = drone_to_trajectory_xy.length();
|
|
|
|
|
|
|
|
|
|
float time_stretch = 1.f - math::constrain(position_error * 0.5f, 0.f, 1.f);
|
|
|
|
|
|
|
|
|
|
// Don't stretch time if the drone is ahead of the position setpoint
|
|
|
|
|
if (drone_to_trajectory_xy.dot(vel_traj_xy) < 0.f) {
|
|
|
|
|
time_stretch = 1.f;
|
|
|
|
|
}
|
|
|
|
|
|
2018-10-25 15:29:45 +02:00
|
|
|
Vector3f jerk_sp_smooth;
|
|
|
|
|
Vector3f accel_sp_smooth;
|
|
|
|
|
Vector3f vel_sp_smooth;
|
|
|
|
|
Vector3f pos_sp_smooth;
|
2018-10-23 14:06:40 +02:00
|
|
|
|
|
|
|
|
for (int i = 0; i < 3; ++i) {
|
2018-10-25 15:29:45 +02:00
|
|
|
_trajectory[i].integrate(_deltatime, time_stretch, accel_sp_smooth(i), vel_sp_smooth(i), pos_sp_smooth(i));
|
|
|
|
|
jerk_sp_smooth(i) = _trajectory[i].getCurrentJerk();
|
2018-10-23 14:06:40 +02:00
|
|
|
}
|
2018-10-25 15:29:45 +02:00
|
|
|
|
|
|
|
|
_updateTrajConstraints();
|
|
|
|
|
|
2019-05-09 14:09:15 +02:00
|
|
|
// If the acceleration and velocities are small and that we want to stop, reduce the amplitude of the jerk signal
|
|
|
|
|
// to help the optimizer to converge towards zero
|
|
|
|
|
if (Vector2f(_velocity_setpoint).length() < (0.01f * _param_mpc_xy_traj_p.get())
|
|
|
|
|
&& Vector2f(accel_sp_smooth).length() < 0.2f
|
|
|
|
|
&& Vector2f(vel_sp_smooth).length() < 0.1f) {
|
|
|
|
|
_trajectory[0].setMaxJerk(1.f);
|
|
|
|
|
_trajectory[1].setMaxJerk(1.f);
|
|
|
|
|
}
|
|
|
|
|
|
2018-10-25 15:29:45 +02:00
|
|
|
for (int i = 0; i < 3; ++i) {
|
|
|
|
|
_trajectory[i].updateDurations(_deltatime, _velocity_setpoint(i));
|
|
|
|
|
}
|
|
|
|
|
|
|
|
|
|
VelocitySmoothing::timeSynchronization(_trajectory, 2); // Synchronize x and y only
|
|
|
|
|
|
|
|
|
|
_jerk_setpoint = jerk_sp_smooth;
|
|
|
|
|
_acceleration_setpoint = accel_sp_smooth;
|
|
|
|
|
_velocity_setpoint = vel_sp_smooth;
|
|
|
|
|
_position_setpoint = pos_sp_smooth;
|
2018-10-23 14:06:40 +02:00
|
|
|
}
|