uuv_att_control_params.c
3.67 KB
1
2
3
4
5
6
7
8
9
10
11
12
13
14
15
16
17
18
19
20
21
22
23
24
25
26
27
28
29
30
31
32
33
34
35
36
37
38
39
40
41
42
43
44
45
46
47
48
49
50
51
52
53
54
55
56
57
58
59
60
61
62
63
64
65
66
67
68
69
70
71
72
73
74
75
76
77
78
79
80
81
82
83
84
85
86
87
88
89
90
91
92
93
94
95
96
97
98
99
100
101
102
103
104
105
106
107
108
109
110
111
112
113
114
115
116
117
118
119
120
121
122
123
124
125
126
127
128
129
130
131
132
133
134
135
136
137
138
139
140
141
142
143
144
/****************************************************************************
*
* Copyright (c) 2013-2020 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 uuv_att_control_params.c
*
* Parameters defined by the attitude control task for unmanned underwater vehicles (UUVs)
*
* This is a modification of the fixed wing/ground rover params and it is designed for ground rovers.
* It has been developed starting from the fw module, simplified and improved with dedicated items.
*
* All the ackowledgments and credits for the fw wing/rover app are reported in those files.
*
* @author Daniel Duecker <daniel.duecker@tuhh.de>
*/
/*
* Controller parameters, accessible via MAVLink
*
*/
// Roll gains
/**
* Roll proportional gain
*
* @group UUV Attitude Control
*/
PARAM_DEFINE_FLOAT(UUV_ROLL_P, 4.0f);
/**
* Roll differential gain
*
* @group UUV Attitude Control
*/
PARAM_DEFINE_FLOAT(UUV_ROLL_D, 1.5f);
// Pitch gains
/**
* Pitch proportional gain
*
* @group UUV Attitude Control
*/
PARAM_DEFINE_FLOAT(UUV_PITCH_P, 4.0f);
/**
* Pitch differential gain
*
* @group UUV Attitude Control
*/
PARAM_DEFINE_FLOAT(UUV_PITCH_D, 2.0f);
// Yaw gains
/**
* Yawh proportional gain
*
* @group UUV Attitude Control
*/
PARAM_DEFINE_FLOAT(UUV_YAW_P, 4.0f);
/**
* Yaw differential gain
*
* @group UUV Attitude Control
*/
PARAM_DEFINE_FLOAT(UUV_YAW_D, 2.0f);
// Input Modes
/**
* Select Input Mode
*
* @value 0 use Attitude Setpoints
* @value 1 Direct Feedthrough
* @group UUV Attitude Control
*/
PARAM_DEFINE_INT32(UUV_INPUT_MODE, 0);
/**
* Skip the controller
*
* @value 0 use the module's controller
* @value 1 skip the controller and feedthrough the setpoints
*/
PARAM_DEFINE_INT32(UUV_SKIP_CTRL, 0);
/**
* Direct roll input
*
* @group UUV Attitude Control
*/
PARAM_DEFINE_FLOAT(UUV_DIRCT_ROLL, 0.0f);
/**
* Direct pitch input
*
* @group UUV Attitude Control
*/
PARAM_DEFINE_FLOAT(UUV_DIRCT_PITCH, 0.0f);
/**
* Direct yaw input
*
* @group UUV Attitude Control
*/
PARAM_DEFINE_FLOAT(UUV_DIRCT_YAW, 0.0f);
/**
* Direct thrust input
*
* @group UUV Attitude Control
*/
PARAM_DEFINE_FLOAT(UUV_DIRCT_THRUST, 0.0f);