mirror of
https://gitee.com/mirrors_PX4/PX4-Autopilot.git
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Merge branch 'master' of github.com:PX4/Firmware into fw_autoland
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@@ -0,0 +1,38 @@
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############################################################################
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#
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# Copyright (C) 2013 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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# Conversion library
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#
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SRCS = rotation.cpp
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@@ -0,0 +1,62 @@
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/****************************************************************************
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*
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* Copyright (C) 2013 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 rotation.cpp
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*
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* Vector rotation library
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*/
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#include "math.h"
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#include "rotation.h"
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__EXPORT void
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get_rot_matrix(enum Rotation rot, math::Matrix *rot_matrix)
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{
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/* first set to zero */
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rot_matrix->Matrix::zero(3, 3);
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float roll = M_DEG_TO_RAD_F * (float)rot_lookup[rot].roll;
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float pitch = M_DEG_TO_RAD_F * (float)rot_lookup[rot].pitch;
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float yaw = M_DEG_TO_RAD_F * (float)rot_lookup[rot].yaw;
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math::EulerAngles euler(roll, pitch, yaw);
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math::Dcm R(euler);
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for (int i = 0; i < 3; i++) {
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for (int j = 0; j < 3; j++) {
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(*rot_matrix)(i, j) = R(i, j);
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}
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}
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}
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@@ -0,0 +1,121 @@
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/****************************************************************************
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*
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* Copyright (C) 2013 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
|
||||
* 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
|
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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
|
||||
* 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
|
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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 rotation.h
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*
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* Vector rotation library
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*/
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#ifndef ROTATION_H_
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#define ROTATION_H_
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#include <unistd.h>
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#include <mathlib/mathlib.h>
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/**
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* Enum for board and external compass rotations.
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* This enum maps from board attitude to airframe attitude.
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*/
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enum Rotation {
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ROTATION_NONE = 0,
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ROTATION_YAW_45 = 1,
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ROTATION_YAW_90 = 2,
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ROTATION_YAW_135 = 3,
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ROTATION_YAW_180 = 4,
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ROTATION_YAW_225 = 5,
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ROTATION_YAW_270 = 6,
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ROTATION_YAW_315 = 7,
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ROTATION_ROLL_180 = 8,
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ROTATION_ROLL_180_YAW_45 = 9,
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ROTATION_ROLL_180_YAW_90 = 10,
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ROTATION_ROLL_180_YAW_135 = 11,
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ROTATION_PITCH_180 = 12,
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ROTATION_ROLL_180_YAW_225 = 13,
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ROTATION_ROLL_180_YAW_270 = 14,
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ROTATION_ROLL_180_YAW_315 = 15,
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ROTATION_ROLL_90 = 16,
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ROTATION_ROLL_90_YAW_45 = 17,
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ROTATION_ROLL_90_YAW_90 = 18,
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ROTATION_ROLL_90_YAW_135 = 19,
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ROTATION_ROLL_270 = 20,
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ROTATION_ROLL_270_YAW_45 = 21,
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ROTATION_ROLL_270_YAW_90 = 22,
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ROTATION_ROLL_270_YAW_135 = 23,
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ROTATION_PITCH_90 = 24,
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ROTATION_PITCH_270 = 25,
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ROTATION_MAX
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};
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typedef struct {
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uint16_t roll;
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uint16_t pitch;
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uint16_t yaw;
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} rot_lookup_t;
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const rot_lookup_t rot_lookup[] = {
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{ 0, 0, 0 },
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{ 0, 0, 45 },
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{ 0, 0, 90 },
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{ 0, 0, 135 },
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{ 0, 0, 180 },
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{ 0, 0, 225 },
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{ 0, 0, 270 },
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{ 0, 0, 315 },
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{180, 0, 0 },
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{180, 0, 45 },
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{180, 0, 90 },
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{180, 0, 135 },
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{ 0, 180, 0 },
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{180, 0, 225 },
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{180, 0, 270 },
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{180, 0, 315 },
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{ 90, 0, 0 },
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{ 90, 0, 45 },
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{ 90, 0, 90 },
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{ 90, 0, 135 },
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{270, 0, 0 },
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{270, 0, 45 },
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{270, 0, 90 },
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{270, 0, 135 },
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{ 0, 90, 0 },
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{ 0, 270, 0 }
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};
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/**
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* Get the rotation matrix
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*/
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__EXPORT void
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get_rot_matrix(enum Rotation rot, math::Matrix *rot_matrix);
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#endif /* ROTATION_H_ */
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@@ -43,7 +43,7 @@
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float ECL_L1_Pos_Controller::nav_roll()
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{
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float ret = atanf(_lateral_accel * 1.0f / CONSTANTS_ONE_G);
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ret = math::constrain(ret, (-M_PI_F) / 2.0f, M_PI_F / 2.0f);
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ret = math::constrain(ret, -_roll_lim_rad, _roll_lim_rad);
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return ret;
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}
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@@ -222,6 +222,15 @@ public:
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_K_L1 = 4.0f * _L1_damping * _L1_damping;
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}
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/**
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* Set the maximum roll angle output in radians
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*
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*/
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void set_l1_roll_limit(float roll_lim_rad) {
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_roll_lim_rad = roll_lim_rad;
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}
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private:
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float _lateral_accel; ///< Lateral acceleration setpoint in m/s^2
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@@ -238,6 +247,8 @@ private:
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float _K_L1; ///< L1 control gain for _L1_damping
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float _heading_omega; ///< Normalized frequency
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float _roll_lim_rad; ///<maximum roll angle
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/**
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* Convert a 2D vector from WGS84 to planar coordinates.
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*
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