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initial control allocation support
- control allocation module with multirotor, VTOL standard, and tiltrotor support - angular_velocity_controller - See https://github.com/PX4/PX4-Autopilot/pull/13351 for details Co-authored-by: Silvan Fuhrer <silvan@auterion.com> Co-authored-by: Roman Bapst <bapstroman@gmail.com>
This commit is contained in:
committed by
Daniel Agar
parent
fc6b61dad1
commit
343cf5603e
+115
@@ -0,0 +1,115 @@
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/****************************************************************************
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*
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* Copyright (c) 2019 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
|
||||
* 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
|
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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 AngularVelocityControl.cpp
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*/
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#include <AngularVelocityControl.hpp>
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#include <px4_platform_common/defines.h>
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using namespace matrix;
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void AngularVelocityControl::setGains(const Vector3f &P, const Vector3f &I, const Vector3f &D)
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{
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_gain_p = P;
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_gain_i = I;
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_gain_d = D;
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}
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void AngularVelocityControl::setSaturationStatus(const matrix::Vector<bool, 3> &saturation_positive,
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const matrix::Vector<bool, 3> &saturation_negative)
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{
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_saturation_positive = saturation_positive;
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_saturation_negative = saturation_negative;
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}
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void AngularVelocityControl::update(const Vector3f &angular_velocity, const Vector3f &angular_velocity_sp,
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const Vector3f &angular_acceleration, const float dt, const bool landed)
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{
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// angular rates error
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Vector3f angular_velocity_error = angular_velocity_sp - angular_velocity;
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// P + D control
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_angular_accel_sp = _gain_p.emult(angular_velocity_error) - _gain_d.emult(angular_acceleration);
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// I + FF control
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Vector3f torque_feedforward = _angular_velocity_int + _gain_ff.emult(angular_velocity_sp);
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// compute torque setpoint
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_torque_sp = _inertia * _angular_accel_sp + torque_feedforward + angular_velocity.cross(_inertia * angular_velocity);
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// update integral only if we are not landed
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if (!landed) {
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updateIntegral(angular_velocity_error, dt);
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}
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}
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void AngularVelocityControl::updateIntegral(Vector3f &angular_velocity_error, const float dt)
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{
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for (int i = 0; i < 3; i++) {
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// prevent further positive control saturation
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if (_saturation_positive(i)) {
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angular_velocity_error(i) = math::min(angular_velocity_error(i), 0.f);
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}
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// prevent further negative control saturation
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if (_saturation_negative(i)) {
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angular_velocity_error(i) = math::max(angular_velocity_error(i), 0.f);
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}
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// I term factor: reduce the I gain with increasing rate error.
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// This counteracts a non-linear effect where the integral builds up quickly upon a large setpoint
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// change (noticeable in a bounce-back effect after a flip).
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// The formula leads to a gradual decrease w/o steps, while only affecting the cases where it should:
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// with the parameter set to 400 degrees, up to 100 deg rate error, i_factor is almost 1 (having no effect),
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// and up to 200 deg error leads to <25% reduction of I.
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float i_factor = angular_velocity_error(i) / math::radians(400.f);
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i_factor = math::max(0.0f, 1.f - i_factor * i_factor);
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// Perform the integration using a first order method
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float angular_velocity_i = _angular_velocity_int(i) + i_factor * _gain_i(i) * angular_velocity_error(i) * dt;
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// do not propagate the result if out of range or invalid
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if (PX4_ISFINITE(angular_velocity_i)) {
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_angular_velocity_int(i) = math::constrain(angular_velocity_i, -_lim_int(i), _lim_int(i));
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}
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}
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}
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void AngularVelocityControl::reset()
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{
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_angular_velocity_int.zero();
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_torque_sp.zero();
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_angular_accel_sp.zero();
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}
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+149
@@ -0,0 +1,149 @@
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/****************************************************************************
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*
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* Copyright (c) 2019 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
|
||||
* 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.
|
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* 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
|
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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 AngularVelocityControl.hpp
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*
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* PID 3 axis angular velocity control.
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*/
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#pragma once
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#include <matrix/matrix/math.hpp>
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#include <lib/mixer/MultirotorMixer/MultirotorMixer.hpp>
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class AngularVelocityControl
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{
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public:
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AngularVelocityControl() = default;
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~AngularVelocityControl() = default;
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/**
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* Set the control gains
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* @param P 3D vector of proportional gains for body x,y,z axis
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* @param I 3D vector of integral gains
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* @param D 3D vector of derivative gains
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*/
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void setGains(const matrix::Vector3f &P, const matrix::Vector3f &I, const matrix::Vector3f &D);
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/**
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* Set the mximum absolute value of the integrator for all axes
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* @param integrator_limit limit value for all axes x, y, z
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*/
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void setIntegratorLimit(const matrix::Vector3f &integrator_limit) { _lim_int = integrator_limit; };
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/**
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* Set direct angular velocity setpoint to torque feed forward gain
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* @see _gain_ff
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* @param FF 3D vector of feed forward gains for body x,y,z axis
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*/
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void setFeedForwardGain(const matrix::Vector3f &FF) { _gain_ff = FF; };
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/**
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* Set inertia matrix
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* @see _inertia
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* @param inertia inertia matrix
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*/
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void setInertiaMatrix(const matrix::Matrix3f &inertia) { _inertia = inertia; };
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/**
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* Set saturation status
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* @see _saturation_positive
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* @see _saturation_negative
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* @param saturation_positive positive saturation
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* @param saturation_negative negative saturation
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*/
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void setSaturationStatus(const matrix::Vector<bool, 3> &saturation_positive,
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const matrix::Vector<bool, 3> &saturation_negative);
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/**
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* Run one control loop cycle calculation
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* @param angular_velocity estimation of the current vehicle angular velocity
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* @param angular_velocity_sp desired vehicle angular velocity setpoint
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* @param angular_acceleration estimation of the current vehicle angular acceleration
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* @param dt elapsed time since last update
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* @param landed whether the vehicle is on the ground
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*/
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void update(const matrix::Vector3f &angular_velocity, const matrix::Vector3f &angular_velocity_sp,
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const matrix::Vector3f &angular_acceleration, const float dt, const bool landed);
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/**
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* Get the desired angular acceleration
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* @see _angular_accel_sp
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*/
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const matrix::Vector3f &getAngularAccelerationSetpoint() {return _angular_accel_sp;};
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/**
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* Get the torque vector to apply to the vehicle
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* @see _torque_sp
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*/
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const matrix::Vector3f &getTorqueSetpoint() {return _torque_sp;};
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/**
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* Get the integral term
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* @see _torque_sp
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*/
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const matrix::Vector3f &getIntegral() {return _angular_velocity_int;};
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/**
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* Set the integral term to 0 to prevent windup
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* @see _angular_velocity_int
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*/
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void resetIntegral() { _angular_velocity_int.zero(); }
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/**
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* ReSet the controller state
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*/
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void reset();
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private:
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void updateIntegral(matrix::Vector3f &angular_velocity_error, const float dt);
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// Gains
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matrix::Vector3f _gain_p; ///< proportional gain for all axes x, y, z
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matrix::Vector3f _gain_i; ///< integral gain
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matrix::Vector3f _gain_d; ///< derivative gain
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matrix::Vector3f _lim_int; ///< integrator term maximum absolute value
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matrix::Vector3f _gain_ff; ///< direct angular velocity to torque feed forward gain
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matrix::Matrix3f _inertia{matrix::eye<float, 3>()}; ///< inertia matrix
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// States
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matrix::Vector3f _angular_velocity_int;
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matrix::Vector<bool, 3> _saturation_positive;
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matrix::Vector<bool, 3> _saturation_negative;
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// Output
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matrix::Vector3f _angular_accel_sp; //< Angular acceleration setpoint computed using P and D gains
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matrix::Vector3f _torque_sp; //< Torque setpoint to apply to the vehicle
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};
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+45
@@ -0,0 +1,45 @@
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/****************************************************************************
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*
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* Copyright (C) 2019 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
|
||||
* 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
|
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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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#include <gtest/gtest.h>
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#include <AngularVelocityControl.hpp>
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using namespace matrix;
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TEST(AngularVelocityControlTest, AllZeroCase)
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{
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AngularVelocityControl control;
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control.update(Vector3f(), Vector3f(), Vector3f(), 0.f, false);
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Vector3f torque = control.getTorqueSetpoint();
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EXPECT_EQ(torque, Vector3f());
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}
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@@ -0,0 +1,41 @@
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############################################################################
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#
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# Copyright (c) 2019 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:
|
||||
#
|
||||
# 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.
|
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#
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############################################################################
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px4_add_library(AngularVelocityControl
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AngularVelocityControl.cpp
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)
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target_compile_options(AngularVelocityControl PRIVATE ${MAX_CUSTOM_OPT_LEVEL})
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target_include_directories(AngularVelocityControl PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
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target_link_libraries(AngularVelocityControl PRIVATE mathlib)
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px4_add_unit_gtest(SRC AngularVelocityControlTest.cpp LINKLIBS AngularVelocityControl)
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@@ -0,0 +1,344 @@
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/****************************************************************************
|
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*
|
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* Copyright (c) 2013-2019 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.
|
||||
*
|
||||
****************************************************************************/
|
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|
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#include "AngularVelocityController.hpp"
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#include <drivers/drv_hrt.h>
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#include <circuit_breaker/circuit_breaker.h>
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#include <mathlib/math/Limits.hpp>
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#include <mathlib/math/Functions.hpp>
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#include <ecl/geo/geo.h>
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using namespace matrix;
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using namespace time_literals;
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AngularVelocityController::AngularVelocityController() :
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ModuleParams(nullptr),
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WorkItem(MODULE_NAME, px4::wq_configurations::ctrl_alloc),
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_loop_perf(perf_alloc(PC_ELAPSED, MODULE_NAME": cycle"))
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{
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_vehicle_status.vehicle_type = vehicle_status_s::VEHICLE_TYPE_ROTARY_WING;
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parameters_updated();
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}
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AngularVelocityController::~AngularVelocityController()
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{
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perf_free(_loop_perf);
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}
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bool
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AngularVelocityController::init()
|
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{
|
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if (!_vehicle_angular_velocity_sub.registerCallback()) {
|
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PX4_ERR("vehicle_angular_velocity callback registration failed!");
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return false;
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}
|
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return true;
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}
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|
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void
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AngularVelocityController::parameters_updated()
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{
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// Control parameters
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// The controller gain K is used to convert the parallel (P + I/s + sD) form
|
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// to the ideal (K * [1 + 1/sTi + sTd]) form
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const Vector3f k_gains = Vector3f(_param_avc_x_k.get(), _param_avc_y_k.get(), _param_avc_z_k.get());
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_control.setGains(
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k_gains.emult(Vector3f(_param_avc_x_p.get(), _param_avc_y_p.get(), _param_avc_z_p.get())),
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k_gains.emult(Vector3f(_param_avc_x_i.get(), _param_avc_y_i.get(), _param_avc_z_i.get())),
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k_gains.emult(Vector3f(_param_avc_x_d.get(), _param_avc_y_d.get(), _param_avc_z_d.get())));
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_control.setIntegratorLimit(
|
||||
Vector3f(_param_avc_x_i_lim.get(), _param_avc_y_i_lim.get(), _param_avc_z_i_lim.get()));
|
||||
|
||||
_control.setFeedForwardGain(
|
||||
Vector3f(_param_avc_x_ff.get(), _param_avc_y_ff.get(), _param_avc_z_ff.get()));
|
||||
|
||||
// inertia matrix
|
||||
const float inertia[3][3] = {
|
||||
{_param_vm_inertia_xx.get(), _param_vm_inertia_xy.get(), _param_vm_inertia_xz.get()},
|
||||
{_param_vm_inertia_xy.get(), _param_vm_inertia_yy.get(), _param_vm_inertia_yz.get()},
|
||||
{_param_vm_inertia_xz.get(), _param_vm_inertia_yz.get(), _param_vm_inertia_zz.get()}
|
||||
};
|
||||
_control.setInertiaMatrix(matrix::Matrix3f(inertia));
|
||||
|
||||
// Hover thrust
|
||||
if (!_param_mpc_use_hte.get()) {
|
||||
_hover_thrust = _param_mpc_thr_hover.get();
|
||||
}
|
||||
}
|
||||
|
||||
void
|
||||
AngularVelocityController::Run()
|
||||
{
|
||||
if (should_exit()) {
|
||||
_vehicle_angular_velocity_sub.unregisterCallback();
|
||||
exit_and_cleanup();
|
||||
return;
|
||||
}
|
||||
|
||||
perf_begin(_loop_perf);
|
||||
|
||||
// Check if parameters have changed
|
||||
if (_parameter_update_sub.updated()) {
|
||||
// clear update
|
||||
parameter_update_s param_update;
|
||||
_parameter_update_sub.copy(¶m_update);
|
||||
|
||||
updateParams();
|
||||
parameters_updated();
|
||||
}
|
||||
|
||||
/* run controller on gyro changes */
|
||||
vehicle_angular_velocity_s vehicle_angular_velocity;
|
||||
|
||||
if (_vehicle_angular_velocity_sub.update(&vehicle_angular_velocity)) {
|
||||
const hrt_abstime now = hrt_absolute_time();
|
||||
_timestamp_sample = vehicle_angular_velocity.timestamp_sample;
|
||||
|
||||
// Guard against too small (< 0.2ms) and too large (> 20ms) dt's.
|
||||
const float dt = math::constrain(((now - _last_run) / 1e6f), 0.0002f, 0.02f);
|
||||
_last_run = now;
|
||||
|
||||
const Vector3f angular_velocity{vehicle_angular_velocity.xyz};
|
||||
|
||||
/* check for updates in other topics */
|
||||
_vehicle_status_sub.update(&_vehicle_status);
|
||||
_vehicle_control_mode_sub.update(&_vehicle_control_mode);
|
||||
|
||||
if (_vehicle_land_detected_sub.updated()) {
|
||||
vehicle_land_detected_s vehicle_land_detected;
|
||||
|
||||
if (_vehicle_land_detected_sub.copy(&vehicle_land_detected)) {
|
||||
_landed = vehicle_land_detected.landed;
|
||||
_maybe_landed = vehicle_land_detected.maybe_landed;
|
||||
}
|
||||
}
|
||||
|
||||
// Check for updates of hover thrust
|
||||
if (_param_mpc_use_hte.get()) {
|
||||
hover_thrust_estimate_s hte;
|
||||
|
||||
if (_hover_thrust_estimate_sub.update(&hte)) {
|
||||
_hover_thrust = hte.hover_thrust;
|
||||
}
|
||||
}
|
||||
|
||||
// check angular acceleration topic
|
||||
vehicle_angular_acceleration_s vehicle_angular_acceleration;
|
||||
|
||||
if (_vehicle_angular_acceleration_sub.update(&vehicle_angular_acceleration)) {
|
||||
_angular_acceleration = Vector3f(vehicle_angular_acceleration.xyz);
|
||||
}
|
||||
|
||||
// check rates setpoint topic
|
||||
vehicle_rates_setpoint_s vehicle_rates_setpoint;
|
||||
|
||||
if (_vehicle_rates_setpoint_sub.update(&vehicle_rates_setpoint)) {
|
||||
_angular_velocity_sp(0) = vehicle_rates_setpoint.roll;
|
||||
_angular_velocity_sp(1) = vehicle_rates_setpoint.pitch;
|
||||
_angular_velocity_sp(2) = vehicle_rates_setpoint.yaw;
|
||||
_thrust_sp = Vector3f(vehicle_rates_setpoint.thrust_body);
|
||||
|
||||
// Scale _thrust_sp in Newton, assuming _hover_thrust is equivalent to 1G
|
||||
_thrust_sp *= (_param_vm_mass.get() * CONSTANTS_ONE_G / _hover_thrust);
|
||||
}
|
||||
|
||||
// run the controller
|
||||
if (_vehicle_control_mode.flag_control_rates_enabled) {
|
||||
// reset integral if disarmed
|
||||
if (!_vehicle_control_mode.flag_armed || _vehicle_status.vehicle_type != vehicle_status_s::VEHICLE_TYPE_ROTARY_WING) {
|
||||
_control.resetIntegral();
|
||||
}
|
||||
|
||||
// update saturation status from mixer feedback
|
||||
if (_control_allocator_status_sub.updated()) {
|
||||
control_allocator_status_s control_allocator_status;
|
||||
|
||||
if (_control_allocator_status_sub.copy(&control_allocator_status)) {
|
||||
Vector<bool, 3> saturation_positive;
|
||||
Vector<bool, 3> saturation_negative;
|
||||
|
||||
if (not control_allocator_status.torque_setpoint_achieved) {
|
||||
for (size_t i = 0; i < 3; i++) {
|
||||
if (control_allocator_status.unallocated_torque[i] > FLT_EPSILON) {
|
||||
saturation_positive(i) = true;
|
||||
|
||||
} else if (control_allocator_status.unallocated_torque[i] < -FLT_EPSILON) {
|
||||
saturation_negative(i) = true;
|
||||
}
|
||||
}
|
||||
}
|
||||
|
||||
_control.setSaturationStatus(saturation_positive, saturation_negative);
|
||||
}
|
||||
}
|
||||
|
||||
// run rate controller
|
||||
_control.update(angular_velocity, _angular_velocity_sp, _angular_acceleration, dt, _maybe_landed || _landed);
|
||||
|
||||
// publish rate controller status
|
||||
rate_ctrl_status_s rate_ctrl_status{};
|
||||
Vector3f integral = _control.getIntegral();
|
||||
rate_ctrl_status.timestamp = hrt_absolute_time();
|
||||
rate_ctrl_status.rollspeed_integ = integral(0);
|
||||
rate_ctrl_status.pitchspeed_integ = integral(1);
|
||||
rate_ctrl_status.yawspeed_integ = integral(2);
|
||||
_rate_ctrl_status_pub.publish(rate_ctrl_status);
|
||||
|
||||
// publish controller output
|
||||
publish_angular_acceleration_setpoint();
|
||||
publish_torque_setpoint();
|
||||
publish_thrust_setpoint();
|
||||
}
|
||||
}
|
||||
|
||||
perf_end(_loop_perf);
|
||||
}
|
||||
|
||||
void
|
||||
AngularVelocityController::publish_angular_acceleration_setpoint()
|
||||
{
|
||||
Vector3f angular_accel_sp = _control.getAngularAccelerationSetpoint();
|
||||
|
||||
vehicle_angular_acceleration_setpoint_s v_angular_accel_sp = {};
|
||||
v_angular_accel_sp.timestamp = hrt_absolute_time();
|
||||
v_angular_accel_sp.timestamp_sample = _timestamp_sample;
|
||||
v_angular_accel_sp.xyz[0] = (PX4_ISFINITE(angular_accel_sp(0))) ? angular_accel_sp(0) : 0.0f;
|
||||
v_angular_accel_sp.xyz[1] = (PX4_ISFINITE(angular_accel_sp(1))) ? angular_accel_sp(1) : 0.0f;
|
||||
v_angular_accel_sp.xyz[2] = (PX4_ISFINITE(angular_accel_sp(2))) ? angular_accel_sp(2) : 0.0f;
|
||||
|
||||
_vehicle_angular_acceleration_setpoint_pub.publish(v_angular_accel_sp);
|
||||
}
|
||||
|
||||
void
|
||||
AngularVelocityController::publish_torque_setpoint()
|
||||
{
|
||||
Vector3f torque_sp = _control.getTorqueSetpoint();
|
||||
|
||||
vehicle_torque_setpoint_s v_torque_sp = {};
|
||||
v_torque_sp.timestamp = hrt_absolute_time();
|
||||
v_torque_sp.timestamp_sample = _timestamp_sample;
|
||||
v_torque_sp.xyz[0] = (PX4_ISFINITE(torque_sp(0))) ? torque_sp(0) : 0.0f;
|
||||
v_torque_sp.xyz[1] = (PX4_ISFINITE(torque_sp(1))) ? torque_sp(1) : 0.0f;
|
||||
v_torque_sp.xyz[2] = (PX4_ISFINITE(torque_sp(2))) ? torque_sp(2) : 0.0f;
|
||||
|
||||
_vehicle_torque_setpoint_pub.publish(v_torque_sp);
|
||||
}
|
||||
|
||||
void
|
||||
AngularVelocityController::publish_thrust_setpoint()
|
||||
{
|
||||
vehicle_thrust_setpoint_s v_thrust_sp = {};
|
||||
v_thrust_sp.timestamp = hrt_absolute_time();
|
||||
v_thrust_sp.timestamp_sample = _timestamp_sample;
|
||||
v_thrust_sp.xyz[0] = (PX4_ISFINITE(_thrust_sp(0))) ? (_thrust_sp(0)) : 0.0f;
|
||||
v_thrust_sp.xyz[1] = (PX4_ISFINITE(_thrust_sp(1))) ? (_thrust_sp(1)) : 0.0f;
|
||||
v_thrust_sp.xyz[2] = (PX4_ISFINITE(_thrust_sp(2))) ? (_thrust_sp(2)) : 0.0f;
|
||||
|
||||
_vehicle_thrust_setpoint_pub.publish(v_thrust_sp);
|
||||
}
|
||||
|
||||
int AngularVelocityController::task_spawn(int argc, char *argv[])
|
||||
{
|
||||
AngularVelocityController *instance = new AngularVelocityController();
|
||||
|
||||
if (instance) {
|
||||
_object.store(instance);
|
||||
_task_id = task_id_is_work_queue;
|
||||
|
||||
if (instance->init()) {
|
||||
return PX4_OK;
|
||||
}
|
||||
|
||||
} else {
|
||||
PX4_ERR("alloc failed");
|
||||
}
|
||||
|
||||
delete instance;
|
||||
_object.store(nullptr);
|
||||
_task_id = -1;
|
||||
|
||||
return PX4_ERROR;
|
||||
}
|
||||
|
||||
int AngularVelocityController::print_status()
|
||||
{
|
||||
PX4_INFO("Running");
|
||||
|
||||
perf_print_counter(_loop_perf);
|
||||
|
||||
return 0;
|
||||
}
|
||||
|
||||
int AngularVelocityController::custom_command(int argc, char *argv[])
|
||||
{
|
||||
return print_usage("unknown command");
|
||||
}
|
||||
|
||||
int AngularVelocityController::print_usage(const char *reason)
|
||||
{
|
||||
if (reason) {
|
||||
PX4_WARN("%s\n", reason);
|
||||
}
|
||||
|
||||
PRINT_MODULE_DESCRIPTION(
|
||||
R"DESCR_STR(
|
||||
### Description
|
||||
This implements the angular velocity controller.
|
||||
It takes angular velocity setpoints and measured angular
|
||||
velocity as inputs and outputs actuator setpoints.
|
||||
|
||||
The controller has a PID loop for angular rate error.
|
||||
|
||||
)DESCR_STR");
|
||||
|
||||
PRINT_MODULE_USAGE_NAME(MODULE_NAME, "controller");
|
||||
PRINT_MODULE_USAGE_COMMAND("start");
|
||||
PRINT_MODULE_USAGE_DEFAULT_COMMANDS();
|
||||
|
||||
return 0;
|
||||
}
|
||||
|
||||
/**
|
||||
* Angular velocity controller app start / stop handling function
|
||||
*/
|
||||
extern "C" __EXPORT int angular_velocity_controller_main(int argc, char *argv[]);
|
||||
|
||||
int angular_velocity_controller_main(int argc, char *argv[])
|
||||
{
|
||||
return AngularVelocityController::main(argc, argv);
|
||||
}
|
||||
@@ -0,0 +1,177 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2013-2019 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.
|
||||
*
|
||||
****************************************************************************/
|
||||
|
||||
#pragma once
|
||||
|
||||
#include <AngularVelocityControl.hpp>
|
||||
|
||||
#include <lib/mathlib/math/filter/LowPassFilter2pVector3f.hpp>
|
||||
#include <lib/matrix/matrix/math.hpp>
|
||||
#include <lib/perf/perf_counter.h>
|
||||
#include <px4_platform_common/defines.h>
|
||||
#include <px4_platform_common/module.h>
|
||||
#include <px4_platform_common/module_params.h>
|
||||
#include <px4_platform_common/posix.h>
|
||||
#include <px4_platform_common/px4_work_queue/ScheduledWorkItem.hpp>
|
||||
#include <uORB/Publication.hpp>
|
||||
#include <uORB/Subscription.hpp>
|
||||
#include <uORB/SubscriptionCallback.hpp>
|
||||
|
||||
#include <uORB/topics/control_allocator_status.h>
|
||||
#include <uORB/topics/hover_thrust_estimate.h>
|
||||
#include <uORB/topics/parameter_update.h>
|
||||
#include <uORB/topics/rate_ctrl_status.h>
|
||||
#include <uORB/topics/vehicle_angular_acceleration.h>
|
||||
#include <uORB/topics/vehicle_angular_acceleration_setpoint.h>
|
||||
#include <uORB/topics/vehicle_angular_velocity.h>
|
||||
#include <uORB/topics/vehicle_control_mode.h>
|
||||
#include <uORB/topics/vehicle_land_detected.h>
|
||||
#include <uORB/topics/vehicle_rates_setpoint.h>
|
||||
#include <uORB/topics/vehicle_status.h>
|
||||
#include <uORB/topics/vehicle_thrust_setpoint.h>
|
||||
#include <uORB/topics/vehicle_torque_setpoint.h>
|
||||
|
||||
|
||||
class AngularVelocityController : public ModuleBase<AngularVelocityController>, public ModuleParams,
|
||||
public px4::WorkItem
|
||||
{
|
||||
public:
|
||||
AngularVelocityController();
|
||||
|
||||
virtual ~AngularVelocityController();
|
||||
|
||||
/** @see ModuleBase */
|
||||
static int task_spawn(int argc, char *argv[]);
|
||||
|
||||
/** @see ModuleBase */
|
||||
static int custom_command(int argc, char *argv[]);
|
||||
|
||||
/** @see ModuleBase */
|
||||
static int print_usage(const char *reason = nullptr);
|
||||
|
||||
/** @see ModuleBase::print_status() */
|
||||
int print_status() override;
|
||||
|
||||
void Run() override;
|
||||
|
||||
bool init();
|
||||
|
||||
private:
|
||||
|
||||
/**
|
||||
* initialize some vectors/matrices from parameters
|
||||
*/
|
||||
void parameters_updated();
|
||||
|
||||
void vehicle_status_poll();
|
||||
|
||||
void publish_angular_acceleration_setpoint();
|
||||
void publish_torque_setpoint();
|
||||
void publish_thrust_setpoint();
|
||||
void publish_actuator_controls();
|
||||
|
||||
AngularVelocityControl _control; ///< class for control calculations
|
||||
|
||||
uORB::Subscription _control_allocator_status_sub{ORB_ID(control_allocator_status)}; /**< motor limits subscription */
|
||||
uORB::Subscription _parameter_update_sub{ORB_ID(parameter_update)}; /**< parameter updates subscription */
|
||||
uORB::Subscription _vehicle_angular_acceleration_sub{ORB_ID(vehicle_angular_acceleration)}; /**< vehicle angular acceleration subscription */
|
||||
uORB::Subscription _vehicle_control_mode_sub{ORB_ID(vehicle_control_mode)}; /**< vehicle control mode subscription */
|
||||
uORB::Subscription _vehicle_land_detected_sub{ORB_ID(vehicle_land_detected)}; /**< vehicle land detected subscription */
|
||||
uORB::Subscription _vehicle_rates_setpoint_sub{ORB_ID(vehicle_rates_setpoint)}; /**< vehicle rates setpoint subscription */
|
||||
uORB::Subscription _vehicle_status_sub{ORB_ID(vehicle_status)}; /**< vehicle status subscription */
|
||||
uORB::Subscription _hover_thrust_estimate_sub{ORB_ID(hover_thrust_estimate)};
|
||||
|
||||
uORB::SubscriptionCallbackWorkItem _vehicle_angular_velocity_sub{this, ORB_ID(vehicle_angular_velocity)};
|
||||
|
||||
uORB::Publication<rate_ctrl_status_s> _rate_ctrl_status_pub{ORB_ID(rate_ctrl_status)}; /**< controller status publication */
|
||||
uORB::Publication<vehicle_angular_acceleration_setpoint_s> _vehicle_angular_acceleration_setpoint_pub{ORB_ID(vehicle_angular_acceleration_setpoint)}; /**< angular acceleration setpoint publication */
|
||||
uORB::Publication<vehicle_thrust_setpoint_s> _vehicle_thrust_setpoint_pub{ORB_ID(vehicle_thrust_setpoint)}; /**< thrust setpoint publication */
|
||||
uORB::Publication<vehicle_torque_setpoint_s> _vehicle_torque_setpoint_pub{ORB_ID(vehicle_torque_setpoint)}; /**< torque setpoint publication */
|
||||
|
||||
vehicle_control_mode_s _vehicle_control_mode{};
|
||||
vehicle_status_s _vehicle_status{};
|
||||
|
||||
bool _landed{true};
|
||||
bool _maybe_landed{true};
|
||||
|
||||
float _battery_status_scale{0.0f};
|
||||
|
||||
perf_counter_t _loop_perf; /**< loop duration performance counter */
|
||||
|
||||
matrix::Vector3f _angular_velocity_sp; /**< angular velocity setpoint */
|
||||
matrix::Vector3f _angular_acceleration; /**< angular acceleration (estimated) */
|
||||
matrix::Vector3f _thrust_sp; /**< thrust setpoint */
|
||||
|
||||
float _hover_thrust{0.5f}; /**< Normalized hover thrust **/
|
||||
|
||||
bool _gear_state_initialized{false}; /**< true if the gear state has been initialized */
|
||||
|
||||
hrt_abstime _task_start{hrt_absolute_time()};
|
||||
hrt_abstime _last_run{0};
|
||||
hrt_abstime _timestamp_sample{0};
|
||||
|
||||
DEFINE_PARAMETERS(
|
||||
(ParamFloat<px4::params::AVC_X_P>) _param_avc_x_p,
|
||||
(ParamFloat<px4::params::AVC_X_I>) _param_avc_x_i,
|
||||
(ParamFloat<px4::params::AVC_X_I_LIM>) _param_avc_x_i_lim,
|
||||
(ParamFloat<px4::params::AVC_X_D>) _param_avc_x_d,
|
||||
(ParamFloat<px4::params::AVC_X_FF>) _param_avc_x_ff,
|
||||
(ParamFloat<px4::params::AVC_X_K>) _param_avc_x_k,
|
||||
|
||||
(ParamFloat<px4::params::AVC_Y_P>) _param_avc_y_p,
|
||||
(ParamFloat<px4::params::AVC_Y_I>) _param_avc_y_i,
|
||||
(ParamFloat<px4::params::AVC_Y_I_LIM>) _param_avc_y_i_lim,
|
||||
(ParamFloat<px4::params::AVC_Y_D>) _param_avc_y_d,
|
||||
(ParamFloat<px4::params::AVC_Y_FF>) _param_avc_y_ff,
|
||||
(ParamFloat<px4::params::AVC_Y_K>) _param_avc_y_k,
|
||||
|
||||
(ParamFloat<px4::params::AVC_Z_P>) _param_avc_z_p,
|
||||
(ParamFloat<px4::params::AVC_Z_I>) _param_avc_z_i,
|
||||
(ParamFloat<px4::params::AVC_Z_I_LIM>) _param_avc_z_i_lim,
|
||||
(ParamFloat<px4::params::AVC_Z_D>) _param_avc_z_d,
|
||||
(ParamFloat<px4::params::AVC_Z_FF>) _param_avc_z_ff,
|
||||
(ParamFloat<px4::params::AVC_Z_K>) _param_avc_z_k,
|
||||
|
||||
(ParamFloat<px4::params::VM_MASS>) _param_vm_mass,
|
||||
(ParamFloat<px4::params::VM_INERTIA_XX>) _param_vm_inertia_xx,
|
||||
(ParamFloat<px4::params::VM_INERTIA_YY>) _param_vm_inertia_yy,
|
||||
(ParamFloat<px4::params::VM_INERTIA_ZZ>) _param_vm_inertia_zz,
|
||||
(ParamFloat<px4::params::VM_INERTIA_XY>) _param_vm_inertia_xy,
|
||||
(ParamFloat<px4::params::VM_INERTIA_XZ>) _param_vm_inertia_xz,
|
||||
(ParamFloat<px4::params::VM_INERTIA_YZ>) _param_vm_inertia_yz,
|
||||
|
||||
(ParamFloat<px4::params::MPC_THR_HOVER>) _param_mpc_thr_hover,
|
||||
(ParamBool<px4::params::MPC_USE_HTE>) _param_mpc_use_hte
|
||||
)
|
||||
|
||||
};
|
||||
@@ -0,0 +1,49 @@
|
||||
############################################################################
|
||||
#
|
||||
# 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.
|
||||
#
|
||||
############################################################################
|
||||
|
||||
add_subdirectory(AngularVelocityControl)
|
||||
|
||||
px4_add_module(
|
||||
MODULE modules__angular_velocity_control
|
||||
MAIN angular_velocity_controller
|
||||
COMPILE_FLAGS
|
||||
${MAX_CUSTOM_OPT_LEVEL}
|
||||
SRCS
|
||||
AngularVelocityController.cpp
|
||||
AngularVelocityController.hpp
|
||||
DEPENDS
|
||||
circuit_breaker
|
||||
mathlib
|
||||
AngularVelocityControl
|
||||
px4_work_queue
|
||||
)
|
||||
@@ -0,0 +1,297 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2013-2019 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 angular_velocity_controller_params.c
|
||||
* Parameters for angular velocity controller.
|
||||
*
|
||||
* @author Lorenz Meier <lorenz@px4.io>
|
||||
* @author Anton Babushkin <anton@px4.io>
|
||||
* @author Julien Lecoeur <julien.lecoeur@gmail.com>
|
||||
*/
|
||||
|
||||
/**
|
||||
* Body X axis angular velocity P gain
|
||||
*
|
||||
* Body X axis angular velocity proportional gain, i.e. control output for angular speed error 1 rad/s.
|
||||
*
|
||||
* @unit 1/s
|
||||
* @min 0.0
|
||||
* @max 20.0
|
||||
* @decimal 3
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_X_P, 18.f);
|
||||
|
||||
/**
|
||||
* Body X axis angular velocity I gain
|
||||
*
|
||||
* Body X axis angular velocity integral gain. Can be set to compensate static thrust difference or gravity center offset.
|
||||
*
|
||||
* @unit Nm/rad
|
||||
* @min 0.0
|
||||
* @decimal 3
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_X_I, 0.2f);
|
||||
|
||||
/**
|
||||
* Body X axis angular velocity integrator limit
|
||||
*
|
||||
* Body X axis angular velocity integrator limit. Can be set to increase the amount of integrator available to counteract disturbances or reduced to improve settling time after large roll moment trim changes.
|
||||
*
|
||||
* @unit Nm
|
||||
* @min 0.0
|
||||
* @decimal 2
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_X_I_LIM, 0.3f);
|
||||
|
||||
/**
|
||||
* Body X axis angular velocity D gain
|
||||
*
|
||||
* Body X axis angular velocity differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
|
||||
*
|
||||
* @min 0.0
|
||||
* @max 2.0
|
||||
* @decimal 4
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_X_D, 0.36f);
|
||||
|
||||
/**
|
||||
* Body X axis angular velocity feedforward gain
|
||||
*
|
||||
* Improves tracking performance.
|
||||
*
|
||||
* @unit Nm/(rad/s)
|
||||
* @min 0.0
|
||||
* @decimal 4
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_X_FF, 0.0f);
|
||||
|
||||
/**
|
||||
* Body X axis angular velocity controller gain
|
||||
*
|
||||
* Global gain of the controller.
|
||||
*
|
||||
* This gain scales the P, I and D terms of the controller:
|
||||
* output = AVC_X_K * (AVC_X_P * error
|
||||
* + AVC_X_I * error_integral
|
||||
* + AVC_X_D * error_derivative)
|
||||
* Set AVC_X_P=1 to implement a PID in the ideal form.
|
||||
* Set AVC_X_K=1 to implement a PID in the parallel form.
|
||||
*
|
||||
* @min 0.0
|
||||
* @max 5.0
|
||||
* @decimal 4
|
||||
* @increment 0.0005
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_X_K, 1.0f);
|
||||
|
||||
/**
|
||||
* Body Y axis angular velocity P gain
|
||||
*
|
||||
* Body Y axis angular velocity proportional gain, i.e. control output for angular speed error 1 rad/s.
|
||||
*
|
||||
* @unit 1/s
|
||||
* @min 0.0
|
||||
* @max 20.0
|
||||
* @decimal 3
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Y_P, 18.f);
|
||||
|
||||
/**
|
||||
* Body Y axis angular velocity I gain
|
||||
*
|
||||
* Body Y axis angular velocity integral gain. Can be set to compensate static thrust difference or gravity center offset.
|
||||
*
|
||||
* @unit Nm/rad
|
||||
* @min 0.0
|
||||
* @decimal 3
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Y_I, 0.2f);
|
||||
|
||||
/**
|
||||
* Body Y axis angular velocity integrator limit
|
||||
*
|
||||
* Body Y axis angular velocity integrator limit. Can be set to increase the amount of integrator available to counteract disturbances or reduced to improve settling time after large pitch moment trim changes.
|
||||
*
|
||||
* @unit Nm
|
||||
* @min 0.0
|
||||
* @decimal 2
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Y_I_LIM, 0.3f);
|
||||
|
||||
/**
|
||||
* Body Y axis angular velocity D gain
|
||||
*
|
||||
* Body Y axis angular velocity differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
|
||||
*
|
||||
* @min 0.0
|
||||
* @max 2.0
|
||||
* @decimal 4
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Y_D, 0.36f);
|
||||
|
||||
/**
|
||||
* Body Y axis angular velocity feedforward
|
||||
*
|
||||
* Improves tracking performance.
|
||||
*
|
||||
* @unit Nm/(rad/s)
|
||||
* @min 0.0
|
||||
* @decimal 4
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Y_FF, 0.0f);
|
||||
|
||||
/**
|
||||
* Body Y axis angular velocity controller gain
|
||||
*
|
||||
* Global gain of the controller.
|
||||
*
|
||||
* This gain scales the P, I and D terms of the controller:
|
||||
* output = AVC_Y_K * (AVC_Y_P * error
|
||||
* + AVC_Y_I * error_integral
|
||||
* + AVC_Y_D * error_derivative)
|
||||
* Set AVC_Y_P=1 to implement a PID in the ideal form.
|
||||
* Set AVC_Y_K=1 to implement a PID in the parallel form.
|
||||
*
|
||||
* @min 0.0
|
||||
* @max 20.0
|
||||
* @decimal 4
|
||||
* @increment 0.0005
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Y_K, 1.0f);
|
||||
|
||||
/**
|
||||
* Body Z axis angular velocity P gain
|
||||
*
|
||||
* Body Z axis angular velocity proportional gain, i.e. control output for angular speed error 1 rad/s.
|
||||
*
|
||||
* @unit 1/s
|
||||
* @min 0.0
|
||||
* @max 20.0
|
||||
* @decimal 2
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Z_P, 7.f);
|
||||
|
||||
/**
|
||||
* Body Z axis angular velocity I gain
|
||||
*
|
||||
* Body Z axis angular velocity integral gain. Can be set to compensate static thrust difference or gravity center offset.
|
||||
*
|
||||
* @unit Nm/rad
|
||||
* @min 0.0
|
||||
* @decimal 2
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Z_I, 0.1f);
|
||||
|
||||
/**
|
||||
* Body Z axis angular velocity integrator limit
|
||||
*
|
||||
* Body Z axis angular velocity integrator limit. Can be set to increase the amount of integrator available to counteract disturbances or reduced to improve settling time after large yaw moment trim changes.
|
||||
*
|
||||
* @unit Nm
|
||||
* @min 0.0
|
||||
* @decimal 2
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Z_I_LIM, 0.30f);
|
||||
|
||||
/**
|
||||
* Body Z axis angular velocity D gain
|
||||
*
|
||||
* Body Z axis angular velocity differential gain. Small values help reduce fast oscillations. If value is too big oscillations will appear again.
|
||||
*
|
||||
* @min 0.0
|
||||
* @max 2.0
|
||||
* @decimal 2
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Z_D, 0.0f);
|
||||
|
||||
/**
|
||||
* Body Z axis angular velocity feedforward
|
||||
*
|
||||
* Improves tracking performance.
|
||||
*
|
||||
* @unit Nm/(rad/s)
|
||||
* @min 0.0
|
||||
* @decimal 4
|
||||
* @increment 0.01
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Z_FF, 0.0f);
|
||||
|
||||
/**
|
||||
* Body Z axis angular velocity controller gain
|
||||
*
|
||||
* Global gain of the controller.
|
||||
*
|
||||
* This gain scales the P, I and D terms of the controller:
|
||||
* output = AVC_Z_K * (AVC_Z_P * error
|
||||
* + AVC_Z_I * error_integral
|
||||
* + AVC_Z_D * error_derivative)
|
||||
* Set AVC_Z_P=1 to implement a PID in the ideal form.
|
||||
* Set AVC_Z_K=1 to implement a PID in the parallel form.
|
||||
*
|
||||
* @min 0.0
|
||||
* @max 5.0
|
||||
* @decimal 4
|
||||
* @increment 0.0005
|
||||
* @group Angular Velocity Control
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(AVC_Z_K, 1.0f);
|
||||
@@ -0,0 +1,109 @@
|
||||
/****************************************************************************
|
||||
*
|
||||
* Copyright (c) 2013-2019 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 vehicle_model_params.c
|
||||
* Parameters for vehicle model.
|
||||
*
|
||||
* @author Julien Lecoeur <julien.lecoeur@gmail.com>
|
||||
*/
|
||||
|
||||
/**
|
||||
* Mass
|
||||
*
|
||||
* @unit kg
|
||||
* @decimal 5
|
||||
* @increment 0.00001
|
||||
* @group Vehicle Model
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(VM_MASS, 1.f);
|
||||
|
||||
/**
|
||||
* Inertia matrix, XX component
|
||||
*
|
||||
* @unit kg m^2
|
||||
* @decimal 5
|
||||
* @increment 0.00001
|
||||
* @group Vehicle Model
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(VM_INERTIA_XX, 0.01f);
|
||||
|
||||
/**
|
||||
* Inertia matrix, YY component
|
||||
*
|
||||
* @unit kg m^2
|
||||
* @decimal 5
|
||||
* @increment 0.00001
|
||||
* @group Vehicle Model
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(VM_INERTIA_YY, 0.01f);
|
||||
|
||||
/**
|
||||
* Inertia matrix, ZZ component
|
||||
*
|
||||
* @unit kg m^2
|
||||
* @decimal 5
|
||||
* @increment 0.00001
|
||||
* @group Vehicle Model
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(VM_INERTIA_ZZ, 0.01f);
|
||||
|
||||
/**
|
||||
* Inertia matrix, XY component
|
||||
*
|
||||
* @unit kg m^2
|
||||
* @decimal 5
|
||||
* @increment 0.00001
|
||||
* @group Vehicle Model
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(VM_INERTIA_XY, 0.f);
|
||||
|
||||
/**
|
||||
* Inertia matrix, XZ component
|
||||
*
|
||||
* @unit kg m^2
|
||||
* @decimal 5
|
||||
* @increment 0.00001
|
||||
* @group Vehicle Model
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(VM_INERTIA_XZ, 0.f);
|
||||
|
||||
/**
|
||||
* Inertia matrix, YZ component
|
||||
*
|
||||
* @unit kg m^2
|
||||
* @decimal 5
|
||||
* @increment 0.00001
|
||||
* @group Vehicle Model
|
||||
*/
|
||||
PARAM_DEFINE_FLOAT(VM_INERTIA_YZ, 0.f);
|
||||
Reference in New Issue
Block a user