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https://gitee.com/mirrors_PX4/PX4-Autopilot.git
synced 2026-10-15 06:03:34 +08:00
Add fw indi lib
F WIP Unit tests
This commit is contained in:
@@ -62,6 +62,7 @@ add_subdirectory(motion_planning EXCLUDE_FROM_ALL)
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add_subdirectory(npfg EXCLUDE_FROM_ALL)
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add_subdirectory(perf EXCLUDE_FROM_ALL)
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add_subdirectory(fw_performance_model EXCLUDE_FROM_ALL)
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add_subdirectory(fw_indi_control EXCLUDE_FROM_ALL)
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add_subdirectory(pid EXCLUDE_FROM_ALL)
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add_subdirectory(pid_design EXCLUDE_FROM_ALL)
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add_subdirectory(pure_pursuit EXCLUDE_FROM_ALL)
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@@ -0,0 +1,42 @@
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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:
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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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px4_add_library(FixedWingIndiControl
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fw_indi_control.cpp
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fw_indi_control.hpp
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)
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target_compile_options(FixedWingIndiControl PRIVATE ${MAX_CUSTOM_OPT_LEVEL})
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target_include_directories(FixedWingIndiControl PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
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target_link_libraries(FixedWingIndiControl PRIVATE mathlib)
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px4_add_unit_gtest(SRC fw_indi_control_test.cpp LINKLIBS FixedWingIndiControl)
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@@ -0,0 +1,89 @@
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/****************************************************************************
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*
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* Copyright (c) 2019-2023 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 rate_control.cpp
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*/
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#include "fw_indi_control.hpp"
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#include <px4_platform_common/defines.h>
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using namespace matrix;
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Quatf
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FixedWingIndiControl::get_flat_attitude(Vector3f vel, Vector3f f)
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{
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const Vector3f vel_air = vel - wind_estimate_;
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// compute force component projected onto lift axis
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const Vector3f vel_normalized = vel_air.normalized();
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Vector3f f_drag = (f * vel_normalized) * vel_normalized;
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Vector3f f_lift = f - f_drag;
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const Vector3f lift_normalized = f_lift.normalized();
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const Vector3f wing_normalized = -vel_normalized.cross(lift_normalized);
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// compute rotation matrix between ENU and FRD frame
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Dcmf R_bi;
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R_bi(0, 0) = vel_normalized(0);
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R_bi(0, 1) = vel_normalized(1);
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R_bi(0, 2) = vel_normalized(2);
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R_bi(1, 0) = wing_normalized(0);
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R_bi(1, 1) = wing_normalized(1);
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R_bi(1, 2) = wing_normalized(2);
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R_bi(2, 0) = lift_normalized(0);
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R_bi(2, 1) = lift_normalized(1);
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R_bi(2, 2) = lift_normalized(2);
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R_bi.renormalize();
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float rho_corrected;
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if (_cal_airspeed >= _stall_speed) {
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rho_corrected = _rho * powf(_cal_airspeed / _true_airspeed, 2);
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} else {
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rho_corrected = _rho;
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}
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// compute required AoA
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Vector3f f_phi = R_bi * f_lift;
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float AoA = ((2.f * f_phi(2)) / (rho_corrected * _area * (vel_air * vel_air) + 0.001f) - _C_L0) / _C_L1 - _aoa_offset;
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// compute final rotation matrix
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Eulerf e(0.f, AoA, 0.f);
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Dcmf R_pitch(e);
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Dcmf Rotation(R_pitch * R_bi);
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Quatf q(Rotation);
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return q;
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}
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@@ -0,0 +1,75 @@
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/****************************************************************************
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*
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* Copyright (c) 2019-2023 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 rate_control.hpp
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*
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* PID 3 axis angular rate / 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 <mathlib/mathlib.h>
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#include <uORB/topics/rate_ctrl_status.h>
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class FixedWingIndiControl
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{
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public:
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FixedWingIndiControl() = default;
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~FixedWingIndiControl() = default;
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void set_coefficients(float area, float aoa_offset, float C_L0, float C_L1) {
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_area = area;
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_aoa_offset = aoa_offset;
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_C_L0 = C_L0;
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_C_L1 = C_L1;
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}
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matrix::Quatf get_flat_attitude(matrix::Vector3f vel, matrix::Vector3f f);
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private:
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// Airdata
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matrix::Vector3f wind_estimate_;
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float _cal_airspeed;
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float _stall_speed;
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float _true_airspeed;
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float _rho{1.0f};
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// Model parameters
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float _area{0.4f};
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float _C_L0{0.3f};
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float _C_L1{2.354f};
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float _aoa_offset{0.07f};
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};
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@@ -0,0 +1,47 @@
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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:
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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.
|
||||
* 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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#include <gtest/gtest.h>
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#include <lib/fw_indi_control/fw_indi_control.hpp>
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using namespace matrix;
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TEST(FixedWingIndiControlTest, AllZeroCase)
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{
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FixedWingIndiControl indi_control;
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Vector3f forward_vel{10.0, 0.0, 0.0};
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Vector3f f_command{0.0, 0.0, 10.0};
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indi_control.set_coefficients(1.0, 0.0, 0.0, 1.0);
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Quatf attitude = indi_control.get_flat_attitude(forward_vel, f_command);
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EXPECT_EQ(attitude, Quatf());
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}
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@@ -39,6 +39,6 @@ px4_add_module(
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FixedwingIndiPosControl.hpp
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DEPENDS
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px4_work_queue
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RateControl
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FixedWingIndiControl
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SlewRate
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)
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@@ -162,7 +162,7 @@ private:
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matrix::Quatf vehicle_attitude_;
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float _cal_airspeed{0.0f};
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float _rho{1.0};
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float _rho{1.225f};
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float _true_airspeed{1.0};
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@@ -205,8 +205,6 @@ private:
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(ParamFloat<px4::params::FW_INDI_K_PITCH>) _param_rot_k_pitch
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)
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RateControl _rate_control; ///< class for rate control calculations
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/**
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* Update our local parameter cache.
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*/
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