bc0e912 | tomaso_de_ponti | 03 July 2024, 13:46:38 UTC | clean up of flightplan plus transition in line before circle with new icons | 03 July 2024, 13:46:38 UTC |
ff259ec | tomaso_de_ponti | 03 July 2024, 09:35:19 UTC | armonize flight plan | 03 July 2024, 09:35:19 UTC |
5500033 | tomaso_de_ponti | 03 July 2024, 09:34:57 UTC | incidence angle of ele in oneloop ctrl | 03 July 2024, 09:34:57 UTC |
5ee3d39 | tomaso_de_ponti | 03 July 2024, 08:55:09 UTC | alignement fix | 03 July 2024, 08:55:09 UTC |
f0a95d2 | tomaso_de_ponti | 03 July 2024, 08:42:33 UTC | added incidence angle scheduling for the elevator | 03 July 2024, 08:42:33 UTC |
5258679 | tomaso_de_ponti | 26 June 2024, 07:50:21 UTC | Log debug fast | 26 June 2024, 07:50:21 UTC |
3c89cad | tomaso_de_ponti | 25 June 2024, 11:34:22 UTC | Added slider to increase the minimum deflection of the elevator | 25 June 2024, 11:34:22 UTC |
86bd72a | tomaso_de_ponti | 25 June 2024, 11:33:25 UTC | Pitch control test plot | 25 June 2024, 11:33:25 UTC |
d74f140 | tomaso_de_ponti | 25 June 2024, 11:07:34 UTC | Do not filter airspeed in eff scheduling as it is already filtered. Compute inertia change before computing the other effectivenesses. | 25 June 2024, 11:07:34 UTC |
0b3d867 | tomaso_de_ponti | 25 June 2024, 11:06:18 UTC | use new motor dynamics for slow pole. Debug vector for model prediction. | 25 June 2024, 11:06:18 UTC |
3cc0f64 | tomaso_de_ponti | 25 June 2024, 11:02:54 UTC | increase log speed in simulation | 25 June 2024, 11:02:54 UTC |
77b7e2f | tomaso_de_ponti | 19 June 2024, 14:16:25 UTC | post valkenburgh | 19 June 2024, 14:16:25 UTC |
fa0f615 | tomaso_de_ponti | 18 June 2024, 15:24:47 UTC | small clean up | 18 June 2024, 15:24:47 UTC |
5807be3 | tomaso | 17 June 2024, 09:26:30 UTC | conf sync | 17 June 2024, 09:26:30 UTC |
b0fd0fe | tomaso | 17 June 2024, 09:26:16 UTC | transform optitrack pose in ekf2 to account for the skew angle | 17 June 2024, 09:26:16 UTC |
cda4f48 | tomaso | 17 June 2024, 09:25:13 UTC | Bring up to date ekf2 otptitrack airframe. Use INS ins RW mode | 17 June 2024, 09:25:13 UTC |
348f164 | tomaso | 17 June 2024, 09:24:09 UTC | clean up of extpose code and switch to abi bind for skew measurement | 17 June 2024, 09:24:09 UTC |
17144cf | tomaso | 17 June 2024, 09:16:16 UTC | clean up airframe outdoors | 17 June 2024, 09:16:16 UTC |
4fb97df | tomaso | 14 June 2024, 08:16:04 UTC | conf sync | 14 June 2024, 08:16:04 UTC |
b6a1eb8 | tomaso | 14 June 2024, 08:15:14 UTC | Different skew limit for ailerons and flaps | 14 June 2024, 08:15:14 UTC |
6a05b3b | tomaso | 14 June 2024, 08:14:12 UTC | Extra includes in the flight plans | 14 June 2024, 08:14:12 UTC |
4a354ae | tomaso | 14 June 2024, 08:11:18 UTC | Fixed generated autopilot not running periodic nav functions in some modes | 14 June 2024, 08:11:18 UTC |
e57e3e7 | tomaso | 14 June 2024, 08:08:56 UTC | Harmonization of airframes. New magneto calibration. | 14 June 2024, 08:08:56 UTC |
05b1e6f | tomaso | 12 June 2024, 11:44:18 UTC | no sin when fake airspeed | 12 June 2024, 11:44:18 UTC |
06b8d70 | tomaso | 11 June 2024, 17:06:25 UTC | safety switch small skew for as | 11 June 2024, 17:06:25 UTC |
c0e0540 | tomaso | 11 June 2024, 09:24:03 UTC | If in force forward allow the maximum acceleration | 11 June 2024, 09:24:03 UTC |
32a5603 | tomaso | 11 June 2024, 09:23:35 UTC | Increase maximum airspeed and maximum descent speed. Fixed bug of bounding acc in body not overwriting the variable. Fixed bug of limits of pitch in forward flight swapped around. | 11 June 2024, 09:23:35 UTC |
cd8e364 | tomaso | 11 June 2024, 09:21:56 UTC | added new icon for descent in quad mode | 11 June 2024, 09:21:56 UTC |
d36e225 | tomaso | 11 June 2024, 09:20:46 UTC | added descend block to aid landing before manual take-over | 11 June 2024, 09:20:46 UTC |
46a34a1 | tomaso | 10 June 2024, 11:43:52 UTC | stall protection on also in forward setting state | 10 June 2024, 11:43:52 UTC |
59d7f25 | tomaso | 10 June 2024, 11:42:17 UTC | FIlter skew angle reading for smoother effectiveness | 10 June 2024, 11:42:17 UTC |
878d57a | tomaso | 10 June 2024, 11:41:06 UTC | stall protection in oneloop | 10 June 2024, 11:41:06 UTC |
015f155 | tomaso | 10 June 2024, 11:40:15 UTC | FIlter accelerations at 3hz. Faster quad motor dynamics. | 10 June 2024, 11:40:15 UTC |
d9164ba | tomaso | 07 June 2024, 08:02:13 UTC | Settings changed | 07 June 2024, 08:02:13 UTC |
6286224 | tomaso | 07 June 2024, 08:01:11 UTC | Periodic frequency calculation of effectiveness | 07 June 2024, 08:01:11 UTC |
02cdf94 | tomaso | 07 June 2024, 08:00:09 UTC | RW optitrack skew correction | 07 June 2024, 08:00:09 UTC |
97d618b | tomaso | 05 June 2024, 11:30:42 UTC | FInalized airspeed control andm ade heading not deviate too much | 05 June 2024, 11:30:42 UTC |
3f2da20 | tomaso | 05 June 2024, 11:29:26 UTC | Ele effectiveness slider. New zero ele | 05 June 2024, 11:29:26 UTC |
5cbe8fd | tomaso | 05 June 2024, 11:27:38 UTC | adjusted values of model | 05 June 2024, 11:27:38 UTC |
af3049a | tomaso | 05 June 2024, 11:26:52 UTC | lowered max deceleration | 05 June 2024, 11:26:52 UTC |
be247cf | tomaso | 04 June 2024, 14:06:51 UTC | Rework of circle so that acceleration bound is calculated also in force forward. | 04 June 2024, 14:06:51 UTC |
03c045e | tomaso | 04 June 2024, 14:06:12 UTC | Ele scheduling not zero at root scheduling. Sine on fake airspeed | 04 June 2024, 14:06:12 UTC |
ab4af74 | tomaso | 04 June 2024, 14:05:32 UTC | Complementary filter on angular rate and airspeed control. | 04 June 2024, 14:05:32 UTC |
b9c60c0 | tomaso | 04 June 2024, 14:04:15 UTC | attitude angles in degrees for simulation | 04 June 2024, 14:04:15 UTC |
76a4417 | tomaso | 04 June 2024, 14:03:17 UTC | Update of airframes | 04 June 2024, 14:03:17 UTC |
f04aa92 | tomaso | 29 May 2024, 10:58:22 UTC | smaller accelerations when going to a waypoint. bigger accelerations when close to circle | 29 May 2024, 10:58:22 UTC |
79f86f1 | tomaso | 29 May 2024, 10:57:39 UTC | change gamma following changes in eff ele and cost ele. Vertical speed max can be specified in airframe. Airspeed control as in guidance indi hybrid. | 29 May 2024, 10:57:39 UTC |
de356a3 | tomaso | 29 May 2024, 10:55:49 UTC | ele effective only amfter 8.8 ms in sim. linearly increases until 16. | 29 May 2024, 10:55:49 UTC |
098e4aa | tomaso | 29 May 2024, 10:55:01 UTC | removed temp slider | 29 May 2024, 10:55:01 UTC |
b945e87 | tomaso | 29 May 2024, 10:54:38 UTC | new ele cost also in sim airframe | 29 May 2024, 10:54:38 UTC |
9340812 | tomaso | 29 May 2024, 07:36:19 UTC | removed temp slider on ele cost | 29 May 2024, 07:36:19 UTC |
d5ed4f5 | tomaso | 28 May 2024, 18:45:48 UTC | Post cyberzoo lowered gain on ele cost | 28 May 2024, 18:45:48 UTC |
28254fa | tomaso | 28 May 2024, 17:10:27 UTC | Ele not effective before 8.8 ms. New ele effect. Ele pref scheduled. | 28 May 2024, 17:10:27 UTC |
d889530 | tomaso | 28 May 2024, 17:09:20 UTC | reset psi ref to psi if not in flight. Correct airspeed ctrl tomaso. Lower vertical speed maximum. Do not reset state variables in not in flight. | 28 May 2024, 17:09:20 UTC |
11f36a3 | tomaso | 28 May 2024, 17:05:22 UTC | jsbsim correct dynamics of AS | 28 May 2024, 17:05:22 UTC |
aecc751 | tomaso | 28 May 2024, 17:04:34 UTC | manual ele test slider | 28 May 2024, 17:04:34 UTC |
19d35b9 | tomaso | 28 May 2024, 17:03:51 UTC | New elevator limits, new min inflight thrust, correct dynamics of actuators | 28 May 2024, 17:03:51 UTC |
0386e03 | tomaso | 28 May 2024, 17:01:59 UTC | changed conf | 28 May 2024, 17:01:59 UTC |
319894a | tomaso | 23 May 2024, 10:39:50 UTC | debug message + faster attitude update in model + bigger thrust limit in model | 23 May 2024, 10:39:50 UTC |
3b8b278 | tomaso | 22 May 2024, 17:53:39 UTC | Track iteration number of wls | 22 May 2024, 17:53:39 UTC |
f58cb80 | tomaso | 22 May 2024, 17:52:54 UTC | Adapt code to use new actuator state message. Make sure the de-normalized nu is sent in the message. | 22 May 2024, 17:52:54 UTC |
51f597d | tomaso | 22 May 2024, 17:50:06 UTC | Added new detailed simulation mode. Added message of actuator state | 22 May 2024, 17:50:06 UTC |
1de2adc | tomaso | 22 May 2024, 17:49:15 UTC | Ele preferred state is to be flat | 22 May 2024, 17:49:15 UTC |
c6976c4 | tomaso | 22 May 2024, 15:00:36 UTC | Heading manual offset maximum made larger. Reduced gamma for better A conditioning.Bound airspeed to positive. | 22 May 2024, 15:00:36 UTC |
5a5daf4 | tomaso | 22 May 2024, 14:58:16 UTC | inertia scheduling in jsbsim model | 22 May 2024, 14:58:16 UTC |
20ca118 | tomaso | 21 May 2024, 16:10:31 UTC | test wls | 21 May 2024, 16:10:31 UTC |
3749996 | tomaso | 21 May 2024, 16:09:58 UTC | Normalize also pseudo control vector | 21 May 2024, 16:09:58 UTC |
dfce43f | tomaso | 21 May 2024, 16:09:34 UTC | lighter downlink | 21 May 2024, 16:09:34 UTC |
f746b87 | tomaso | 21 May 2024, 16:09:09 UTC | change weight on aero surf to make them cheap also in sim | 21 May 2024, 16:09:09 UTC |
892527d | tomaso | 21 May 2024, 07:24:05 UTC | fixed primary cost too large wrt secondary cost | 21 May 2024, 07:24:05 UTC |
909680a | tomaso | 15 May 2024, 15:35:41 UTC | split effectiveness matrix in two. code cleanup | 15 May 2024, 15:35:41 UTC |
91c8522 | tomaso | 15 May 2024, 15:34:16 UTC | fake airspeed test | 15 May 2024, 15:34:16 UTC |
2283f44 | Tomaso | 14 May 2024, 13:19:50 UTC | added wls message | 14 May 2024, 13:19:50 UTC |
fc22f77 | Tomaso | 14 May 2024, 13:19:21 UTC | sideslip control post valkenburgh | 14 May 2024, 13:19:21 UTC |
ef4fddf | Tomaso | 08 May 2024, 13:35:04 UTC | goto use nav max speed so is controlled from rotwing state | 08 May 2024, 13:35:04 UTC |
f367459 | Tomaso | 08 May 2024, 10:37:39 UTC | rudementary airspeed control | 08 May 2024, 10:37:39 UTC |
f361b40 | Tomaso | 07 May 2024, 16:56:13 UTC | nav acceleration limit added | 07 May 2024, 16:56:13 UTC |
de375a1 | Tomaso | 07 May 2024, 14:21:04 UTC | post skewing cz test, switch indexmade more clear | 07 May 2024, 14:21:04 UTC |
b51fefc | Tomaso | 06 May 2024, 09:05:16 UTC | Sync conf | 06 May 2024, 09:05:16 UTC |
0b5a59e | Tomaso | 06 May 2024, 09:04:32 UTC | Bring new changes to airframe from simulation to CZ airframe and VB airframe | 06 May 2024, 09:04:32 UTC |
2d2fc64 | Tomaso | 06 May 2024, 09:03:41 UTC | fixed warning | 06 May 2024, 09:03:41 UTC |
2f24306 | Tomaso | 06 May 2024, 08:27:21 UTC | Simulate rot mech dynamics in NPS. Set correctly the guidance H mode in the generated autoplot so that the state machine executes the correct overrides | 06 May 2024, 08:27:21 UTC |
0ff6cf0 | Tomaso | 06 May 2024, 07:36:42 UTC | Fake dynamics rot mech in nps and use rotmech command index in streaming data | 06 May 2024, 07:36:42 UTC |
78f66b9 | Tomaso | 03 May 2024, 09:41:48 UTC | Use index of command for feedback of rotmech | 03 May 2024, 09:41:48 UTC |
977a3ac | Tomaso | 03 May 2024, 09:41:15 UTC | Clean up of eff scheduling | 03 May 2024, 09:41:15 UTC |
ce5355f | Tomaso | 03 May 2024, 09:40:25 UTC | added valkenburgh calib of magneto | 03 May 2024, 09:40:25 UTC |
7d5b990 | Tomaso | 03 May 2024, 08:36:41 UTC | Prevent motor stabilization off in emergency switch back to manual | 03 May 2024, 08:36:41 UTC |
5b5a509 | Tomaso | 03 May 2024, 08:36:01 UTC | new generated autopilot with switch based AP selection | 03 May 2024, 08:36:01 UTC |
01438e8 | Tomaso | 03 May 2024, 08:34:10 UTC | prevent entering nav block and forgetting force skew on | 03 May 2024, 08:34:10 UTC |
d79dda6 | Tomaso | 03 May 2024, 08:31:33 UTC | Added 6ch RC parsing for simulation rw3c | 03 May 2024, 08:31:33 UTC |
32b3434 | Tomaso | 01 May 2024, 14:40:38 UTC | cleaned up flightplan and added icons specific to rw drone | 01 May 2024, 14:40:38 UTC |
d0e096b | Tomaso | 01 May 2024, 09:43:17 UTC | 1) position poles defined in serial. 2) EC position rework to have bounds. 3) Fixed bug moment prediction from the elevator. 4) Switch max limit of quad motors to 0 in forward flight. | 01 May 2024, 09:43:17 UTC |
d98fa62 | Tomaso | 01 May 2024, 09:41:06 UTC | code clean up | 01 May 2024, 09:41:06 UTC |
9811cc6 | Tomaso | 01 May 2024, 09:40:28 UTC | added route between 4 waypoints | 01 May 2024, 09:40:28 UTC |
32dc3cc | Tomaso | 01 May 2024, 09:38:26 UTC | added inertia scheduling to effectiveness scheduling | 01 May 2024, 09:38:26 UTC |
1e8eaa1 | Tomaso | 26 April 2024, 13:02:52 UTC | lower deceleration bound to avoid overshoot | 26 April 2024, 13:02:52 UTC |
72b40bd | Tomaso | 25 April 2024, 09:18:48 UTC | More drag, less aggressive Z in forward flight, actuator based thrust estimation | 25 April 2024, 09:18:48 UTC |
646ce89 | Tomaso | 25 April 2024, 08:21:24 UTC | managed to get simulation to transition, still some oscillations to be fixed. | 25 April 2024, 08:21:24 UTC |
d18373e | Tomaso | 22 April 2024, 12:36:41 UTC | New scheduling, partially tested | 22 April 2024, 12:36:41 UTC |
48e8d7e | Tomaso | 16 April 2024, 16:20:27 UTC | end_of_day | 16 April 2024, 16:20:27 UTC |