/
tudelft_bebop_autonomous_race.xml
210 lines (174 loc) · 7.5 KB
/
tudelft_bebop_autonomous_race.xml
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
145
146
147
148
149
150
151
152
153
154
155
156
157
158
159
160
161
162
163
164
165
166
167
168
169
170
171
172
173
174
175
176
177
178
179
180
181
182
183
184
185
186
187
188
189
190
191
192
193
194
195
196
197
198
199
200
201
202
203
204
205
206
207
208
209
<!DOCTYPE airframe SYSTEM "../airframe.dtd">
<airframe name="bebop">
<firmware name="rotorcraft">
<target name="ap" board="bebop"/>
<target name="nps" board="pc">
<module name="fdm" type="jsbsim"/>
<module name="udp"/>
</target>
<!--define name="USE_SONAR" value="TRUE"/-->
<!-- Subsystem section -->
<module name="telemetry" type="transparent_udp"/>
<module name="radio_control" type="datalink"/>
<module name="motor_mixing"/>
<module name="actuators" type="bebop"/>
<module name="imu" type="bebop"/>
<module name="gps" type="datalink"/>
<module name="stabilization" type="int_quat"/>
<module name="ahrs" type="float_mlkf"/>
<module name="ins" type="extended"/>
</firmware>
<modules main_freq="512">
<module name="geo_mag"/>
<module name="air_data"/>
<module name="send_imu_mag_current"/>
<!--module name="logger_file">
<define name="FILE_LOGGER_PATH" value="/data/ftp/internal_000"/>
</module-->
<module name="video_thread">
</module>
<module name="sonar_bebop"/>
<module name="cv_opticflow">
<define name="OPTICFLOW_METHOD" value="1"/>
<define name="OPTICFLOW_CAMERA" value="bottom_camera"/>
<define name="CAMERA_ROTATED_180" value="TRUE"/>
</module>
<module name="video_rtp_stream">
<define name="VIEWVIDEO_CAMERA" value="bottom_camera"/>
</module>
</modules>
<commands>
<axis name="PITCH" failsafe_value="0"/>
<axis name="ROLL" failsafe_value="0"/>
<axis name="YAW" failsafe_value="0"/>
<axis name="THRUST" failsafe_value="6000"/>
</commands>
<servos driver="Default">
<servo name="TOP_LEFT" no="0" min="3000" neutral="3000" max="12000"/>
<servo name="TOP_RIGHT" no="1" min="3000" neutral="3000" max="12000"/>
<servo name="BOTTOM_RIGHT" no="2" min="3000" neutral="3000" max="12000"/>
<servo name="BOTTOM_LEFT" no="3" min="3000" neutral="3000" max="12000"/>
</servos>
<section name="MIXING" prefix="MOTOR_MIXING_">
<!-- Time cross layout (X), with order NW (CW), NE (CCW), SE (CW), SW (CCW) -->
<define name="TYPE" value="QUAD_X"/>
</section>
<command_laws>
<call fun="motor_mixing_run(autopilot_motors_on,FALSE,values)"/>
<set servo="TOP_LEFT" value="motor_mixing.commands[MOTOR_FRONT_LEFT]"/>
<set servo="TOP_RIGHT" value="motor_mixing.commands[MOTOR_FRONT_RIGHT]"/>
<set servo="BOTTOM_RIGHT" value="motor_mixing.commands[MOTOR_BACK_RIGHT]"/>
<set servo="BOTTOM_LEFT" value="motor_mixing.commands[MOTOR_BACK_LEFT]"/>
</command_laws>
<section name="AIR_DATA" prefix="AIR_DATA_">
<define name="CALC_AIRSPEED" value="FALSE"/>
<define name="CALC_TAS_FACTOR" value="FALSE"/>
<define name="CALC_AMSL_BARO" value="TRUE"/>
</section>
<section name="IMU" prefix="IMU_">
<!-- Magneto calibration -->
<define name="MAG_X_NEUTRAL" value="166"/>
<define name="MAG_Y_NEUTRAL" value="21"/>
<define name="MAG_Z_NEUTRAL" value="202"/>
<define name="MAG_X_SENS" value="6.90518428178" integer="16"/>
<define name="MAG_Y_SENS" value="7.14998083717" integer="16"/>
<define name="MAG_Z_SENS" value="6.91930289812" integer="16"/>
<!-- Magneto current calibration -->
<define name="MAG_X_CURRENT_COEF" value="0.0"/>
<define name="MAG_Y_CURRENT_COEF" value="0.0"/>
<define name="MAG_Z_CURRENT_COEF" value="0.0"/>
<define name="BODY_TO_IMU_PHI" value="0." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
</section>
<!-- local magnetic field -->
<!-- http://wiki.paparazziuav.org/wiki/Subsystem/ahrs#Local_Magnetic_Field -->
<section name="AHRS" prefix="AHRS_">
<!-- values used if no GPS fix, on 3D fix is update by geo_mag module -->
<!-- Delft -->
<define name="H_X" value="0.3892503"/>
<define name="H_Y" value="0.0017972"/>
<define name="H_Z" value="0.9211303"/>
<!-- For vibrating airfames -->
<define name="GRAVITY_HEURISTIC_FACTOR" value="0"/>
</section>
<section name="INS" prefix="INS_">
<define name="SONAR_MAX_RANGE" value="2.2"/>
<define name="SONAR_UPDATE_ON_AGL" value="TRUE"/>
</section>
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- setpoints -->
<define name="SP_MAX_PHI" value="45" unit="deg"/>
<define name="SP_MAX_THETA" value="45" unit="deg"/>
<define name="SP_MAX_R" value="300" unit="deg/s"/>
<define name="DEADBAND_A" value="0"/>
<define name="DEADBAND_E" value="0"/>
<define name="DEADBAND_R" value="50"/>
<!-- reference -->
<define name="REF_OMEGA_P" value="450" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.9"/>
<define name="REF_MAX_P" value="600." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(8000.)"/>
<define name="REF_OMEGA_Q" value="450" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.9"/>
<define name="REF_MAX_Q" value="600." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(8000.)"/>
<define name="REF_OMEGA_R" value="450" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.9"/>
<define name="REF_MAX_R" value="600." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(8000.)"/>
<!-- feedback -->
<define name="PHI_PGAIN" value="920"/>
<define name="PHI_DGAIN" value="425"/>
<define name="PHI_IGAIN" value="0"/>
<define name="THETA_PGAIN" value="920"/>
<define name="THETA_DGAIN" value="425"/>
<define name="THETA_IGAIN" value="0"/>
<define name="PSI_PGAIN" value="8000"/>
<define name="PSI_DGAIN" value="700"/>
<define name="PSI_IGAIN" value="0"/>
<!-- feedforward -->
<define name="PHI_DDGAIN" value="0"/>
<define name="THETA_DDGAIN" value="0"/>
<define name="PSI_DDGAIN" value="0"/>
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
<define name="HOVER_KP" value="550"/>
<define name="HOVER_KD" value="82"/>
<define name="HOVER_KI" value="13"/>
<define name="NOMINAL_HOVER_THROTTLE" value="0.655"/>
<define name="ADAPT_THROTTLE_ENABLED" value="TRUE"/>
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<!-- Good weather -->
<define name="MAX_BANK" value="20" unit="deg"/>
<!-- Bad weather -->
<!-- define name="MAX_BANK" value="32" unit="deg"/ -->
<define name="PGAIN" value="350"/>
<define name="DGAIN" value="100"/>
<define name="IGAIN" value="30"/>
<define name="REF_MAX_SPEED" value="0.2"/>
</section>
<section name="NAVIGATION" prefix="NAV_">
<define name="CLIMB_VSPEED" value="2.5" />
<define name="DESCEND_VSPEED" value="-1.0" />
</section>
<section name="SIMULATOR" prefix="NPS_">
<define name="ACTUATOR_NAMES" value="nw_motor, ne_motor, se_motor, sw_motor" type="string[]"/>
<define name="JSBSIM_MODEL" value="simple_x_quad_ccw" type="string"/>
<define name="SENSORS_PARAMS" value="nps_sensors_params_default.h" type="string"/>
</section>
<section name="AUTOPILOT">
<define name="MODE_STARTUP" value="AP_MODE_NAV"/>
<define name="MODE_MANUAL" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_AUTO1" value="AP_MODE_ATTITUDE_Z_HOLD"/>
<define name="MODE_AUTO2" value="AP_MODE_GUIDED"/>
</section>
<section name="BAT">
<define name="MILLIAMP_AT_FULL_THROTTLE" value="8700"/>
<define name="CATASTROPHIC_BAT_LEVEL" value="9.3" unit="V"/>
<define name="CRITIC_BAT_LEVEL" value="9.6" unit="V"/>
<define name="LOW_BAT_LEVEL" value="10.6" unit="V"/>
<define name="MAX_BAT_LEVEL" value="12.4" unit="V"/>
</section>
</airframe>