Add fw indi lib

F

WIP Unit tests
This commit is contained in:
JaeyoungLim
2025-07-07 15:47:16 +09:00
parent 3e63aec18d
commit c297e6ba76
7 changed files with 256 additions and 4 deletions
+1
View File
@@ -62,6 +62,7 @@ add_subdirectory(motion_planning EXCLUDE_FROM_ALL)
add_subdirectory(npfg EXCLUDE_FROM_ALL)
add_subdirectory(perf EXCLUDE_FROM_ALL)
add_subdirectory(fw_performance_model EXCLUDE_FROM_ALL)
add_subdirectory(fw_indi_control EXCLUDE_FROM_ALL)
add_subdirectory(pid EXCLUDE_FROM_ALL)
add_subdirectory(pid_design EXCLUDE_FROM_ALL)
add_subdirectory(pure_pursuit EXCLUDE_FROM_ALL)
+42
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@@ -0,0 +1,42 @@
############################################################################
#
# 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.
#
############################################################################
px4_add_library(FixedWingIndiControl
fw_indi_control.cpp
fw_indi_control.hpp
)
target_compile_options(FixedWingIndiControl PRIVATE ${MAX_CUSTOM_OPT_LEVEL})
target_include_directories(FixedWingIndiControl PUBLIC ${CMAKE_CURRENT_SOURCE_DIR})
target_link_libraries(FixedWingIndiControl PRIVATE mathlib)
px4_add_unit_gtest(SRC fw_indi_control_test.cpp LINKLIBS FixedWingIndiControl)
@@ -0,0 +1,89 @@
/****************************************************************************
*
* Copyright (c) 2019-2023 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 rate_control.cpp
*/
#include "fw_indi_control.hpp"
#include <px4_platform_common/defines.h>
using namespace matrix;
Quatf
FixedWingIndiControl::get_flat_attitude(Vector3f vel, Vector3f f)
{
const Vector3f vel_air = vel - wind_estimate_;
// compute force component projected onto lift axis
const Vector3f vel_normalized = vel_air.normalized();
Vector3f f_drag = (f * vel_normalized) * vel_normalized;
Vector3f f_lift = f - f_drag;
const Vector3f lift_normalized = f_lift.normalized();
const Vector3f wing_normalized = -vel_normalized.cross(lift_normalized);
// compute rotation matrix between ENU and FRD frame
Dcmf R_bi;
R_bi(0, 0) = vel_normalized(0);
R_bi(0, 1) = vel_normalized(1);
R_bi(0, 2) = vel_normalized(2);
R_bi(1, 0) = wing_normalized(0);
R_bi(1, 1) = wing_normalized(1);
R_bi(1, 2) = wing_normalized(2);
R_bi(2, 0) = lift_normalized(0);
R_bi(2, 1) = lift_normalized(1);
R_bi(2, 2) = lift_normalized(2);
R_bi.renormalize();
float rho_corrected;
if (_cal_airspeed >= _stall_speed) {
rho_corrected = _rho * powf(_cal_airspeed / _true_airspeed, 2);
} else {
rho_corrected = _rho;
}
// compute required AoA
Vector3f f_phi = R_bi * f_lift;
float AoA = ((2.f * f_phi(2)) / (rho_corrected * _area * (vel_air * vel_air) + 0.001f) - _C_L0) / _C_L1 - _aoa_offset;
// compute final rotation matrix
Eulerf e(0.f, AoA, 0.f);
Dcmf R_pitch(e);
Dcmf Rotation(R_pitch * R_bi);
Quatf q(Rotation);
return q;
}
@@ -0,0 +1,75 @@
/****************************************************************************
*
* Copyright (c) 2019-2023 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 rate_control.hpp
*
* PID 3 axis angular rate / angular velocity control.
*/
#pragma once
#include <matrix/matrix/math.hpp>
#include <mathlib/mathlib.h>
#include <uORB/topics/rate_ctrl_status.h>
class FixedWingIndiControl
{
public:
FixedWingIndiControl() = default;
~FixedWingIndiControl() = default;
void set_coefficients(float area, float aoa_offset, float C_L0, float C_L1) {
_area = area;
_aoa_offset = aoa_offset;
_C_L0 = C_L0;
_C_L1 = C_L1;
}
matrix::Quatf get_flat_attitude(matrix::Vector3f vel, matrix::Vector3f f);
private:
// Airdata
matrix::Vector3f wind_estimate_;
float _cal_airspeed;
float _stall_speed;
float _true_airspeed;
float _rho{1.0f};
// Model parameters
float _area{0.4f};
float _C_L0{0.3f};
float _C_L1{2.354f};
float _aoa_offset{0.07f};
};
@@ -0,0 +1,47 @@
/****************************************************************************
*
* 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.
*
****************************************************************************/
#include <gtest/gtest.h>
#include <lib/fw_indi_control/fw_indi_control.hpp>
using namespace matrix;
TEST(FixedWingIndiControlTest, AllZeroCase)
{
FixedWingIndiControl indi_control;
Vector3f forward_vel{10.0, 0.0, 0.0};
Vector3f f_command{0.0, 0.0, 10.0};
indi_control.set_coefficients(1.0, 0.0, 0.0, 1.0);
Quatf attitude = indi_control.get_flat_attitude(forward_vel, f_command);
EXPECT_EQ(attitude, Quatf());
}
@@ -39,6 +39,6 @@ px4_add_module(
FixedwingIndiPosControl.hpp
DEPENDS
px4_work_queue
RateControl
FixedWingIndiControl
SlewRate
)
@@ -162,7 +162,7 @@ private:
matrix::Quatf vehicle_attitude_;
float _cal_airspeed{0.0f};
float _rho{1.0};
float _rho{1.225f};
float _true_airspeed{1.0};
@@ -205,8 +205,6 @@ private:
(ParamFloat<px4::params::FW_INDI_K_PITCH>) _param_rot_k_pitch
)
RateControl _rate_control; ///< class for rate control calculations
/**
* Update our local parameter cache.
*/