-
Notifications
You must be signed in to change notification settings - Fork 1.1k
/
rot_wing_25kg.xml
497 lines (419 loc) · 26.3 KB
/
rot_wing_25kg.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
210
211
212
213
214
215
216
217
218
219
220
221
222
223
224
225
226
227
228
229
230
231
232
233
234
235
236
237
238
239
240
241
242
243
244
245
246
247
248
249
250
251
252
253
254
255
256
257
258
259
260
261
262
263
264
265
266
267
268
269
270
271
272
273
274
275
276
277
278
279
280
281
282
283
284
285
286
287
288
289
290
291
292
293
294
295
296
297
298
299
300
301
302
303
304
305
306
307
308
309
310
311
312
313
314
315
316
317
318
319
320
321
322
323
324
325
326
327
328
329
330
331
332
333
334
335
336
337
338
339
340
341
342
343
344
345
346
347
348
349
350
351
352
353
354
355
356
357
358
359
360
361
362
363
364
365
366
367
368
369
370
371
372
373
374
375
376
377
378
379
380
381
382
383
384
385
386
387
388
389
390
391
392
393
394
395
396
397
398
399
400
401
402
403
404
405
406
407
408
409
410
411
412
413
414
415
416
417
418
419
420
421
422
423
424
425
426
427
428
429
430
431
432
433
434
435
436
437
438
439
440
441
442
443
444
445
446
447
448
449
450
451
452
453
454
455
456
457
458
459
460
461
462
463
464
465
466
467
468
469
470
471
472
473
474
475
476
477
478
479
480
481
482
483
484
485
486
487
488
489
490
491
492
493
494
495
496
497
<!-- This is a Rotating Wing 25kg
* Airframe: TUD00???
* Autopilot: Cube Orange Plus
* Datalink: Herelink
* GPS: UBlox F9P (2x)
* RC: SBUS Crossfire (diversity)
-->
<airframe name="RotatingWing25Kg">
<description>RotatingWing25Kg</description>
<firmware name="rotorcraft">
<target name="ap" board="cube_orangeplus">
<configure name="PERIODIC_FREQUENCY" value="500"/> <!-- Configure the main periodic frequency to 500Hz -->
<module name="radio_control" type="sbus">
<configure name="SBUS_PORT" value="UART3"/> <!-- On the TELEM2 port -->
</module>
<module name="sys_mon"/>
<module name="flight_recorder"/>
<!-- RC switches -->
<define name="RADIO_TH_HOLD" value="RADIO_AUX1"/>
<define name="RADIO_KILL_SWITCH" value="RADIO_AUX1"/>
<define name="RADIO_FMODE" value="RADIO_AUX2"/>
<define name="RADIO_FBW_MODE" value="RADIO_AUX3"/>
<define name="RADIO_CONTROL_THRUST_X" value="RADIO_AUX4"/>
<!-- EKF2 configure inputs -->
<define name="INS_EKF2_GYRO_ID" value="IMU_CUBE1_ID"/>
<define name="INS_EKF2_ACCEL_ID" value="IMU_CUBE1_ID"/>
<define name="INS_EKF2_MAG_ID" value="MAG_RM3100_SENDER_ID"/>
<!--Only send gyro and accel that is being used-->
<define name="IMU_GYRO_ABI_SEND_ID" value= "IMU_CUBE1_ID"/>
<define name="IMU_ACCEL_ABI_SEND_ID" value= "IMU_CUBE1_ID"/>
<!-- Range sensor connected to supercan -->
<module name="range_sensor_uavcan"/>
<!-- Disable current sensing using UAVCAN -->
<define name="UAVCAN_ACTUATORS_USE_CURRENT" value="FALSE"/>
<define name="USE_I2C1"/>
<!-- Log in high speed (Remove for outdoor flights) -->
<!-- <define name="IMU_LOG_HIGHSPEED" value="TRUE"/> -->
</target>
<target name="nps" board="pc">
<module name="radio_control" type="datalink"/>
<module name="fdm" type="jsbsim"/>
<!--Not dealing with these in the simulation-->
<define name="RADIO_TH_HOLD" value="0"/> <!-- Throttle hold in command laws -->
<define name="RADIO_FMODE" value="0"/> <!-- Throttle curve select -->
<define name="RADIO_FBW_MODE" value="0"/> <!-- Switch between AP and FBW control -->
<define name="RADIO_KILL_SWITCH" value="0"/>
<define name="RADIO_CONTROL_THRUST_X" value="0"/>
</target>
<!-- Herelink datalink -->
<module name="telemetry" type="transparent">
<configure name="MODEM_BAUD" value="B460800"/>
</module>
<!-- Sensors -->
<module name="mag" type="rm3100">
<define name="MODULE_RM3100_UPDATE_AHRS" value="TRUE"/>
<configure name="MAG_RM3100_I2C_DEV" value="I2C2"/>
</module>
<module name="airspeed" type="ms45xx_i2c">
<define name="MS45XX_I2C_DEV" value="i2c1"/>
<define name="MS45XX_AIRSPEED_SCALE" value="2.0833"/>
<define name="USE_AIRSPEED_LOWPASS_FILTER" value="TRUE"/>
<define name="MS45XX_LOWPASS_TAU" value="0.15"/>
</module>
<module name="airspeed" type="uavcan">
<define name="AIRSPEED_UAVCAN_LOWPASS_FILTER" value="TRUE" />
<define name="AIRSPEED_UAVCAN_LOWPASS_PERIOD" value="0.1" />
<define name="AIRSPEED_UAVCAN_SEND_ABI" value="0" /> <!-- Read Airspeed for logging but do not use it -->
</module>
<module name="air_data"/>
<module name="gps" type="ublox">
<configure name="UBX_GPS_BAUD" value="B460800"/>
<define name="USE_GPS_UBX_RTCM" value="TRUE"/>
</module>
<!-- IMU / INS -->
<module name="imu" type="cube"/>
<module name="ins" type="ekf2">
<!-- The Cube is mounted 25cm backwards of the CG -->
<define name="INS_EKF2_IMU_POS_X" value="-0.25"/>
<define name="INS_EKF2_IMU_POS_Y" value="0.0"/>
<define name="INS_EKF2_IMU_POS_Z" value="0.0"/>
<!-- The main GPS is mounted at the tail 1.44m backwards and 20cm above the CG -->
<define name="INS_EKF2_GPS_POS_X" value="-1.44"/>
<define name="INS_EKF2_GPS_POS_Y" value="0.0"/>
<define name="INS_EKF2_GPS_POS_Z" value="0.2"/>
</module>
<!-- Actuators on dual CAN bus -->
<module name="actuators" type="uavcan">
<configure value="TRUE" name="UAVCAN_USE_CAN1"/>
<configure value="TRUE" name="UAVCAN_USE_CAN2"/>
</module>
<!-- Control -->
<module name="stabilization" type="indi">
<configure name="INDI_NUM_ACT" value="9"/>
<configure name="INDI_OUTPUTS" value="5"/>
<define name="WLS_N_U" value="9"/>
<define name="WLS_N_V" value="5"/>
</module>
<module name="stabilization" type="rate_indi"/>
<module name="eff_scheduling_rot_wing"/>
<module name="guidance" type="indi_hybrid_quadplane"/>
<module name="nav" type="hybrid">
<define name="GUIDANCE_H_USE_REF" value="FALSE"/>
</module>
<!-- Other -->
<module name="sys_id_doublet"/>
<module name="sys_id_auto_doublets"/>
<module name="rot_wing_automation"/>
<module name="ground_detect_sensor"/>
<module name="rotwing_state"/>
<module name="preflight_checks">
<define name="SDLOG_PREFLIGHT_ERROR" value="TRUE"/>
</module>
<module name="agl_dist"/>
<module name="approach_moving_target"/>
</firmware>
<!-- Can bus 1 actuators -->
<servos driver="Uavcan1">
<servo no="0" name="MOTOR_FRONT" min="-8191" neutral="-5000" max="8191"/>
<servo no="1" name="MOTOR_RIGHT" min="-8191" neutral="-5000" max="8191"/>
<servo no="2" name="MOTOR_BACK" min="-8191" neutral="-5000" max="8191"/>
<servo no="3" name="MOTOR_LEFT" min="-8191" neutral="-5000" max="8191"/>
<servo no="4" name="MOTOR_PUSH" min="-8191" neutral="-8191" max="8191"/>
<servo no="5" name="SERVO_ELEVATOR" min="-3191" neutral="-3191" max="4900"/>
<servo no="6" name="SERVO_RUDDER" min="-6500" neutral="0" max="6500"/>
<servo no="7" name="ROTATION_MECH" min="8191" neutral="0" max="-8191"/>
<servo no="8" name="AIL_RIGHT" min="-8000" neutral="-1000" max="5000"/>
<servo no="9" name="FLAP_RIGHT" min="-8000" neutral="-1000" max="5000"/>
<servo no="10" name="AIL_LEFT" min="-5000" neutral="1000" max="8000"/>
<servo no="11" name="FLAP_LEFT" min="-5000" neutral="1000" max="8000"/>
<servo no="12" name="PARACHUTE" min="-8191" neutral="0" max="8191"/>
</servos>
<!-- Can bus 2 actuators -->
<servos driver="Uavcan2">
<servo no="0" name="BMOTOR_FRONT" min="-8191" neutral="-5000" max="8191"/>
<servo no="1" name="BMOTOR_RIGHT" min="-8191" neutral="-5000" max="8191"/>
<servo no="2" name="BMOTOR_BACK" min="-8191" neutral="-5000" max="8191"/>
<servo no="3" name="BMOTOR_LEFT" min="-8191" neutral="-5000" max="8191"/>
<servo no="4" name="BMOTOR_PUSH" min="-8191" neutral="-8191" max="8191"/>
<servo no="5" name="BSERVO_ELEVATOR" min="-3191" neutral="-3191" max="4900"/>
<servo no="6" name="BSERVO_RUDDER" min="-6500" neutral="0" max="6500"/>
<servo no="7" name="BROTATION_MECH" min="8191" neutral="0" max="-8191"/>
<servo no="8" name="BAIL_RIGHT" min="-8000" neutral="-1000" max="5000"/>
<servo no="9" name="BFLAP_RIGHT" min="-8000" neutral="-1000" max="5000"/>
<servo no="10" name="BAIL_LEFT" min="-5000" neutral="1000" max="8000"/>
<servo no="11" name="BFLAP_LEFT" min="-5000" neutral="1000" max="8000"/>
<servo no="12" name="BPARACHUTE" min="-8191" neutral="0" max="8191"/>
</servos>
<commands>
<axis name="ROLL" failsafe_value="0"/>
<axis name="PITCH" failsafe_value="0"/>
<axis name="YAW" failsafe_value="0"/>
<axis name="THRUST" failsafe_value="0"/>
<axis name="THRUST_X" failsafe_value="0"/>
</commands>
<command_laws>
<let var="th_hold" value="Or(LessThan(RadioControlValues(RADIO_TH_HOLD), -4800), !autopilot_get_motors_on())"/>
<let VAR="servo_hold" VALUE="LessThan(RadioControlValues(RADIO_TH_HOLD), -4800)"/>
<let VAR="hover_off" VALUE="Or($th_hold, bool_disable_hover_motors)"/>
<call fun="sys_id_doublet_add_values(autopilot_get_motors_on(),FALSE,actuators_pprz)"/>
<!-- Main bus -->
<set servo="MOTOR_FRONT" value="($hover_off? -9600 : actuators_pprz[0])"/>
<set servo="MOTOR_RIGHT" value="($hover_off? -9600 : actuators_pprz[1])"/>
<set servo="MOTOR_BACK" value="($hover_off? -9600 : actuators_pprz[2])"/>
<set servo="MOTOR_LEFT" value="($hover_off? -9600 : actuators_pprz[3])"/>
<set servo="MOTOR_PUSH" value="($th_hold? -9600 : actuators_pprz[8])"/>
<set servo="SERVO_ELEVATOR" value="($servo_hold? (RadioControlValues(RADIO_PITCH)/4+7200) : (!autopilot_in_flight()? 0 : actuators_pprz[5]))"/>
<set servo="SERVO_RUDDER" value="($servo_hold? RadioControlValues(RADIO_YAW) : (!autopilot_in_flight()? 0 : actuators_pprz[4]))"/>
<set servo="ROTATION_MECH" value="rotwing_state_skewing.servo_pprz_cmd"/>
<set servo="AIL_RIGHT" value="($servo_hold? RadioControlValues(RADIO_ROLL) : actuators_pprz[6])"/>
<set servo="FLAP_RIGHT" value="($servo_hold? RadioControlValues(RADIO_ROLL) : actuators_pprz[7])"/>
<set servo="AIL_LEFT" value="($servo_hold? RadioControlValues(RADIO_ROLL) : actuators_pprz[6])"/>
<set servo="FLAP_LEFT" value="($servo_hold? RadioControlValues(RADIO_ROLL) : actuators_pprz[7])"/>
<set servo="PARACHUTE" value="RadioControlValues(RADIO_AUX6)"/>
<!-- Second bus -->
<set servo="BMOTOR_FRONT" value="($hover_off? -9600 : actuators_pprz[0])"/>
<set servo="BMOTOR_RIGHT" value="($hover_off? -9600 : actuators_pprz[1])"/>
<set servo="BMOTOR_BACK" value="($hover_off? -9600 : actuators_pprz[2])"/>
<set servo="BMOTOR_LEFT" value="($hover_off? -9600 : actuators_pprz[3])"/>
<set servo="BMOTOR_PUSH" value="($th_hold? -9600 : actuators_pprz[8])"/>
<set servo="BSERVO_ELEVATOR" value="($servo_hold? (RadioControlValues(RADIO_PITCH)/4+7200) : (!autopilot_in_flight()? 0 : actuators_pprz[5]))"/>
<set servo="BSERVO_RUDDER" value="($servo_hold? RadioControlValues(RADIO_YAW) : (!autopilot_in_flight()? 0 : actuators_pprz[4]))"/>
<set servo="BROTATION_MECH" value="rotwing_state_skewing.servo_pprz_cmd"/>
<set servo="BAIL_RIGHT" value="($servo_hold? RadioControlValues(RADIO_ROLL) : actuators_pprz[6])"/>
<set servo="BFLAP_RIGHT" value="($servo_hold? RadioControlValues(RADIO_ROLL) : actuators_pprz[7])"/>
<set servo="BAIL_LEFT" value="($servo_hold? RadioControlValues(RADIO_ROLL) : actuators_pprz[6])"/>
<set servo="BFLAP_LEFT" value="($servo_hold? RadioControlValues(RADIO_ROLL) : actuators_pprz[7])"/>
<set servo="BPARACHUTE" value="RadioControlValues(RADIO_AUX6)"/>
</command_laws>
<section PREFIX="SYS_ID_" NAME="SYS_ID">
<define name="DOUBLET_AXES" value="{0,1,2,3,4,5,6,7,8}"/>
<define name="DOUBLET_RADIO_CHANNEL" value="6"/>
<define name="AUTO_DOUBLETS_N_ACTUATORS" value="4"/>
<define name="AUTO_DOUBLETS_ACTUATORS" value="{0,1,2,3}"/>
<define name="AUTO_DOUBLETS_AMPLITUDE" value="{1500,1500,1500,1500}"/>
<define name="CHIRP_AXES" value="{0,1,2,3}"/>
<define name="CHIRP_RADIO_CHANNEL" value="9"/>
</section>
<section name="CTRL_EFF_SHED" prefix="ROT_WING_EFF_SCHED_">
<define name="IXX_BODY" value="0.2845"/>
<define name="IYY_BODY" value="5.078"/>
<define name="IZZ" value="7.051"/>
<define name="IXX_WING" value="0.712"/>
<define name="IYY_WING" value="1.77"/>
<define name="M" value="25.5"/>
<define name="DM_DPPRZ_HOVER_PITCH" value="0.00925"/>
<define name="DM_DPPRZ_HOVER_ROLL" value="0.0085"/>
<define name="HOVER_ROLL_PITCH_COEF" value="{0.015, -0.011}"/>
<define name="HOVER_ROLL_ROLL_COEF" value="{0.0, -0.0}"/>
<define name="K_ELEVATOR" value="{ 1.27655, -13.3525, -96.0}"/>
<define name="K_RUDDER" value="{-72.5037, -0.9329, -3.23651}"/>
<define name="K_AILERON" value="2.777647188"/>
<define name="K_FLAPERON" value="2.0439"/>
<define name="K_PUSHER" value="{0.027775,-2.41146}"/>
<define name="K_ELEVATOR_DEFLECTION" value="{50.0,-0.0063}"/>
<define name="D_RUDDER_D_PPRZ" value="-0.0018"/>
<define name="K_RPM_PPRZ_PUSHER" value="{-131.497033952591,1.32098226269777,-0.0000291178067445214}"/>
<define name="K_LIFT_WING" value="{-0.335811392,-0.615611143}"/>
<define name="K_LIFT_FUSELAGE" value="-0.050653927"/>
<define name="K_LIFT_TAIL" value="-0.101691751"/>
</section>
<section name="MISC">
<!-- Voltage and current measurements -->
<define name="VoltageOfAdc(adc)" value="((3.3f/65536.0f) * 21.314 * adc)"/> <!-- ADC calibration -->
<define name="MilliAmpereOfAdc(adc)" value="((3.3f/65536.0f) * 50000.f * adc)"/> <!-- Has like a -2A offset -->
<define name="MilliAmpereOfAdc2(adc)" value="((3.3f/65536.0f) * 50000.f * adc)"/> <!-- Seems te be ok -->
<define name="VBoardOfAdc(adc)" value="((3.3f/65536.0f) * 1.89036 * adc)"/>
<define name="ADC_CHANNEL_CURRENT2" value="ADC_4"/>
<!-- Others -->
<define name="NO_RC_THRUST_LIMIT" value="TRUE"/>
<define name="NAV_CLIMB_VSPEED" value="2.0" />
<define name="NAV_DESCEND_VSPEED" value="-1.0"/>
<define name="NAV_CARROT_DIST" value="200"/>
<define name="AUTOPILOT_IN_FLIGHT_MIN_THRUST" value="300"/>
<define name="ARRIVED_AT_WAYPOINT" value="50.0"/>
<define name="NO_GPS_LOST_WITH_DATALINK_TIME" value="20"/>
<define name="NO_GPS_LOST_WITH_RC_VALID" value="TRUE"/>
<define name="USE_AIRSPEED" value="TRUE"/>
<define name="NAV_HYBRID_MAX_DECELERATION" value="0.5"/>
</section>
<section name="GROUND_DETECT">
<define name="THRESHOLD_GROUND_DETECT" value="40"/>
<define name="USE_GROUND_DETECT_INDI_THRUST" value="TRUE"/>
<define name="USE_GROUND_DETECT_AGL_DIST" value="TRUE"/>
<define name="GROUND_DETECT_SENSOR_AGL_MIN_VALUE" value="0.24"/>
<!-- <define name="AGL_DIST_MIN_DISTANCE_CHECK" value="0.20"/>
<define name="AGL_DIST_MAX_DISTANCE_CHECK" value="0.25"/> -->
<define name="AGL_DIST_FILTER" value="0.07"/>
</section>
<section name="IMU" prefix="IMU_">
<define name="ACCEL_CALIB" value="{{.abi_id=20, .calibrated={.neutral=true, .scale=true, .filter=true},.neutral={-3,3,13}, .scale={{15146,60067,2567},{1551,6124,263}}, .filter_sample_freq=1138.7, .filter_freq=30}, {.abi_id=22, .calibrated={.neutral=true, .scale=true, .filter=true},.neutral={-26,9,2}, .scale={{32863,18346,55169},{6721,3745,11294}}, .filter_sample_freq=1139.3, .filter_freq=30}}"/>
<define name="MAG_CALIB" value="{{.abi_id=5, .calibrated={.neutral=true, .scale=true},.neutral={-96,-95,-292}, .scale={{33136,8709,8764},{59233,15343,15761}}}}"/> <!-- Calibrated 't Harde 17-08-2023 -->
<define name="GYRO_CALIB" value="{{.abi_id=20, .calibrated={.filter=true}, .filter_sample_freq=1138.7, .filter_freq=30}, {.abi_id=22, .calibrated={.filter=true}, .filter_sample_freq=1139.3, .filter_freq=30}}"/>
<!-- Define axis in hover frame -->
<define name="BODY_TO_IMU_PHI" value="180." unit="deg"/>
<define name="BODY_TO_IMU_THETA" value="0." unit="deg"/>
<define name="BODY_TO_IMU_PSI" value="0." unit="deg"/>
</section>
<section name="MAG_RM3100" prefix="RM3100_">
<define name="MAG_TO_IMU_PHI" value="-90.0"/>
<define name="MAG_TO_IMU_THETA" value="0.0"/>
<define name="MAG_TO_IMU_PSI" value="0.0"/>
</section>
<section name="STABILIZATION_ATTITUDE" prefix="STABILIZATION_ATTITUDE_">
<!-- Limits -->
<define name="SP_MAX_PHI" value="45." unit="deg" />
<define name="SP_MAX_THETA" value="45." unit="deg"/>
<define name="SP_MAX_R" value="90." unit="deg/s"/>
<define name="DEADBAND_R" value="200"/>
<define name="SP_PSI_DELTA_LIMIT" value="45" unit="deg"/>
<!-- Reference model -->
<define name="REF_OMEGA_P" value="800" unit="deg/s"/>
<define name="REF_ZETA_P" value="0.85"/>
<define name="REF_MAX_P" value="300." unit="deg/s"/>
<define name="REF_MAX_PDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_Q" value="800" unit="deg/s"/>
<define name="REF_ZETA_Q" value="0.85"/>
<define name="REF_MAX_Q" value="300." unit="deg/s"/>
<define name="REF_MAX_QDOT" value="RadOfDeg(7000.)"/>
<define name="REF_OMEGA_R" value="500" unit="deg/s"/>
<define name="REF_ZETA_R" value="0.85"/>
<define name="REF_MAX_R" value="180." unit="deg/s"/>
<define name="REF_MAX_RDOT" value="RadOfDeg(1800.)"/>
<!-- Gains -->
<define name="PHI_PGAIN" value="500"/>
<define name="PHI_DGAIN" value="230"/>
<define name="PHI_IGAIN" value="10"/>
<define name="PHI_DDGAIN" value="0"/>
<define name="THETA_PGAIN" value="500"/>
<define name="THETA_DGAIN" value="230"/>
<define name="THETA_IGAIN" value="10"/>
<define name="THETA_DDGAIN" value="0"/>
<define name="PSI_PGAIN" value="700"/>
<define name="PSI_DGAIN" value="200"/>
<define name="PSI_IGAIN" value="10"/>
<define name="PSI_DDGAIN" value="0"/>
</section>
<section name="STABILIZATION_ATTITUDE_INDI" prefix="STABILIZATION_INDI_">
<!-- G1 and G2 25 kg-->
<define name="G1_ROLL" value="{ 0.0, -9.0, 0.0, 9.0, 0.0, 0.0, 0.0, 0.0, 0.0}"/>
<define name="G1_PITCH" value="{ 1.14, 0.0, -1.14, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0}"/>
<define name="G1_YAW" value="{ -0.29, 0.29, -0.29, 0.29, 0.0, 0.0, 0.0, 0.0, 0.0}"/>
<define name="G1_THRUST" value="{ -0.54, -0.54, -0.54, -0.54, 0.0, 0.0, 0.0, 0.0, 0.0}"/>
<define name="G1_THRUST_X" value="{ 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.9}"/>
<define name="G2" value="{ 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0, 0.0}"/>
<!-- Actuator dynamics -->
<define name="ACT_FREQ" value="{12.1, 12.1, 12.1, 12.1, 52.7, 52.7, 52.7, 52.7, 24.1}"/>
<define name="ACT_IS_SERVO" value="{ 0, 0, 0, 0, 1, 1, 1, 1, 0}"/>
<define name="ACT_IS_THRUSTER_X" value="{ 0, 0, 0, 0, 0, 0, 0, 0, 1}" />
<define VALUE="{1000, 1000, 1, 100, 100}" NAME="WLS_PRIORITIES"/>
<define VALUE="{1.3, 1.3, 1.3, 1.3, 1.0, 1.0, 1.0, 1.0, 1.0}" NAME="WLS_WU"/>
<!-- Rate INDI -->
<define name="MAX_RATE" value="1.5"/>
<!-- Reference -->
<define name="REF_ERR_P" value="40.0"/>
<define name="REF_ERR_Q" value="25.0"/>
<define name="REF_ERR_R" value="23.0"/>
<define name="REF_RATE_P" value="5.5"/>
<define name="REF_RATE_Q" value="4.5"/>
<define name="REF_RATE_R" value="3.9"/>
<define name="MAX_R" value="30.0" unit="deg/s"/>
<!-- Filters -->
<define name="FILTER_RATES_SECOND_ORDER" value="TRUE" />
<define name="FILT_CUTOFF_P" value="10.0"/>
<define name="FILT_CUTOFF_Q" value="10.0"/>
<define name="FILT_CUTOFF_R" value="5.0"/>
<define name="FILT_CUTOFF" value="2.0"/>
<define name="ESTIMATION_FILT_CUTOFF" value="2.0"/>
<define name="FILTER_YAW_RATE" value="TRUE"/>
<define name="OUTPUT_NOTCH_FILTER" value="FALSE"/>
<define name="OUTPUT_NOTCH_FILTER_CUTOFF_F" value="6.5"/>
<define name="OUTPUT_NOTCH_FILTER_BANDWITDH" value="3.0"/>
<!-- Other -->
<define name="WLS_PRIORITIES" value="{1000, 1000, 1, 100, 100}"/>
<define name="WLS_WU" value="{1.3, 1.3, 1.3, 1.3, 1.0, 1.0, 1.0, 1.0, 1.0}"/>
<define name="USE_ADAPTIVE" value="FALSE"/>
<define name="ADAPTIVE_MU" value="0.001"/>
</section>
<section name="GUIDANCE_V" prefix="GUIDANCE_V_">
<!-- Gains -->
<define name="HOVER_KP" value="310"/>
<define name="HOVER_KD" value="130"/>
<define name="HOVER_KI" value="10"/>
<define name="NOMINAL_HOVER_THROTTLE" value="0.42"/>
<define name="ADAPT_THROTTLE_ENABLED" value="FALSE"/>
<!-- Reference -->
<define name="REF_MIN_ZD" value="-4.0"/> <!-- climb -->
<define name="REF_MAX_ZD" value="4.0"/> <!-- descend -->
</section>
<section name="GUIDANCE_H" prefix="GUIDANCE_H_">
<define name="MAX_BANK" value="20" unit="deg"/>
<define name="USE_SPEED_REF" value="TRUE"/>
<!-- Gains -->
<define name="PGAIN" value="60"/>
<define name="DGAIN" value="100"/>
<define name="IGAIN" value="20"/>
<define name="AGAIN" value="0"/>
</section>
<section name="GUIDANCE_INDI_HYBRID" prefix="GUIDANCE_INDI_">
<!--WLS settings-->
<define name="USE_WLS" value="TRUE"/>
<define name="WLS_PRIORITIES" value="{10., 10., 10.}"/>
<define name="WLS_WU" value="{10., 10., 100., 1.}"/>
<!-- Gains -->
<define name="POS_GAIN" value="0.3"/>
<define name="POS_GAINZ" value="0.5"/>
<define name="SPEED_GAIN" value="0.7"/>
<define name="SPEED_GAINZ" value="0.6"/>
<!-- Other -->
<define name="FILTER_CUTOFF" value="2.0"/>
<define name="HEADING_BANK_GAIN" value="5."/>
<define name="MAX_AIRSPEED" value="19.0"/>
<define name="PITCH_LIFT_EFF" value="0.0"/>
<define name="ZERO_AIRSPEED" value="TRUE"/>
<define name="THRUST_Z_EFF" value="-0.0023"/>
<define name="THRUST_X_EFF" value="0.00055"/>
<define name="NAV_CIRCLE_DIST" value="60."/>
<define name="NAV_LINE_DIST" value="100"/>
<define name="LINE_GAIN" value="0.2"/>
<define name="CLIMB_SPEED_FWD" value="2.0"/>
<define name="DESCEND_SPEED_FWD" value="-3.0"/>
<define name="QUADPLANE" value="TRUE"/>
<define name="MAX_PITCH" value="12"/>
<define name="MIN_PITCH" value="-20"/>
</section>
<section name="FORWARD">
<define name="TURN_AIRSPEED_TH" value="8.0"/> <!-- This is the pitch angle that the drone will have in forward flight, where 0 degrees is hover-->
<define name="TRANSITION_MAX_OFFSET" value="0.0" unit="deg"/>
<define name="GUIDANCE_HEADING_IS_FREE" value="FALSE"/>
</section>
<section name="AMT" prefix="APPROACH_MOVING_TARGET_">
<define name="CUTOFF_FREQ_FILTERS_HZ" value="0.25"/>
<define name="ERR_SLOWDOWN_GAIN" value="0.25" />
<define name="SLOPE" value="60.0"/>
<define name="DISTANCE" value="70.0"/>
<define name="SPEED" value="0.0"/>
</section>
<section name="AUTOPILOT">
<define name="MODE_MANUAL" value="AP_MODE_ATTITUDE_DIRECT"/>
<define name="MODE_AUTO1" value="AP_MODE_RATE_DIRECT"/>
<define name="MODE_AUTO2" value="AP_MODE_NAV"/>
<define name="MODE_STARTUP" value="AP_MODE_NAV"/>
</section>
<section name="BAT">
<define name="CATASTROPHIC_BAT_LEVEL" value="36.0" unit="V"/>
<define name="CRITIC_BAT_LEVEL" value="37.2" unit="V"/>
<define name="LOW_BAT_LEVEL" value="48.4" unit="V"/>
<define name="MAX_BAT_LEVEL" value="50.4" unit="V"/>
<define name="TAKEOFF_BAT_LEVEL" value="48.4" unit="V"/>
<define name="BAT_NB_CELLS" value="12"/>
</section>
<section name="SIMULATOR" prefix="NPS_">
<define name="ACTUATOR_NAMES" value="front_motor, right_motor, back_motor, left_motor, rudder, elevator, aileron, flaperon, pusher" type="string[]"/>
<define name="JSBSIM_MODEL" value="rotwing25" type="string"/>
<define name="SENSORS_PARAMS" value="nps_sensors_params_default.h" type="string"/>
<define name="COMMANDS_NB" value="9"/>
<define name="NO_MOTOR_MIXING" value="TRUE"/>
<define name="JS_AXIS_MODE" value="4"/>
</section>
</airframe>