bresch d47f9f155a MC mixer: replace multirotor_motor_limits by control_allocator_status
CA: fix saturation computation
Since the CA matrix is normalized, the same scale applied to be used when using the effectiveness matrix

MCRateControl: use control_allocator_status to get saturation info
2021-11-09 10:35:10 -05:00

120 lines
4.4 KiB
C++

/****************************************************************************
*
* Copyright (c) 2019 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 RateControl.hpp
*
* PID 3 axis angular rate / angular velocity control.
*/
#pragma once
#include <matrix/matrix/math.hpp>
#include <lib/mixer/MultirotorMixer/MultirotorMixer.hpp>
#include <uORB/topics/rate_ctrl_status.h>
class RateControl
{
public:
RateControl() = default;
~RateControl() = default;
/**
* Set the rate control gains
* @param P 3D vector of proportional gains for body x,y,z axis
* @param I 3D vector of integral gains
* @param D 3D vector of derivative gains
*/
void setGains(const matrix::Vector3f &P, const matrix::Vector3f &I, const matrix::Vector3f &D);
/**
* Set the mximum absolute value of the integrator for all axes
* @param integrator_limit limit value for all axes x, y, z
*/
void setIntegratorLimit(const matrix::Vector3f &integrator_limit) { _lim_int = integrator_limit; };
/**
* Set direct rate to torque feed forward gain
* @see _gain_ff
* @param FF 3D vector of feed forward gains for body x,y,z axis
*/
void setFeedForwardGain(const matrix::Vector3f &FF) { _gain_ff = FF; };
/**
* Set saturation status
* @param control saturation vector from control allocator
*/
void setSaturationStatus(const matrix::Vector<bool, 3> &saturation_positive,
const matrix::Vector<bool, 3> &saturation_negative);
/**
* Run one control loop cycle calculation
* @param rate estimation of the current vehicle angular rate
* @param rate_sp desired vehicle angular rate setpoint
* @param dt desired vehicle angular rate setpoint
* @return [-1,1] normalized torque vector to apply to the vehicle
*/
matrix::Vector3f update(const matrix::Vector3f &rate, const matrix::Vector3f &rate_sp,
const matrix::Vector3f &angular_accel, const float dt, const bool landed);
/**
* Set the integral term to 0 to prevent windup
* @see _rate_int
*/
void resetIntegral() { _rate_int.zero(); }
/**
* Get status message of controller for logging/debugging
* @param rate_ctrl_status status message to fill with internal states
*/
void getRateControlStatus(rate_ctrl_status_s &rate_ctrl_status);
private:
void updateIntegral(matrix::Vector3f &rate_error, const float dt);
// Gains
matrix::Vector3f _gain_p; ///< rate control proportional gain for all axes x, y, z
matrix::Vector3f _gain_i; ///< rate control integral gain
matrix::Vector3f _gain_d; ///< rate control derivative gain
matrix::Vector3f _lim_int; ///< integrator term maximum absolute value
matrix::Vector3f _gain_ff; ///< direct rate to torque feed forward gain only useful for helicopters
// States
matrix::Vector3f _rate_int; ///< integral term of the rate controller
// Feedback from control allocation
matrix::Vector<bool, 3> _control_allocator_saturation_negative;
matrix::Vector<bool, 3> _control_allocator_saturation_positive;
};