Andy Piper
|
02a2c788da
|
AC_AttitudeControl: ensure plane always gets the latest gyro
|
2024-09-26 19:25:33 +10:00 |
Andy Piper
|
829422ecfb
|
AC_AttitudeControl: add commentary about functions which modify the rate loop target
|
2024-09-26 19:25:33 +10:00 |
Leonard Hall
|
ddfccb3098
|
AC_AttitudeControl: Use rate step command
|
2024-09-26 19:25:33 +10:00 |
Andy Piper
|
ff002cba3f
|
AC_AttitudeControl: ensure the rate and attitude controllers can't interfere with the target at the same time
|
2024-09-26 19:25:33 +10:00 |
Andy Piper
|
71e2b756af
|
AC_AttitudeControl: introduce ANG log message for high resolution attitude logging
Move RATE message to AC_AttitudeControl_Logging.cpp
|
2024-09-17 10:12:35 +10:00 |
Leonard Hall
|
ea226637c9
|
AC_AttitudeControl: Vector3f multiplication clean up
|
2024-09-17 09:59:55 +10:00 |
Leonard Hall
|
5e27e3111d
|
AC_AttitudeControl: Fix dt update order
|
2024-09-17 09:59:55 +10:00 |
Andy Piper
|
bb2249f766
|
AC_AttitudeControl: record latest gyro value and time used for logging
move Write_Rate() to AC_AttitudeControl
move RATE log structure to AC_AttitudeControl
|
2024-09-10 16:33:04 +01:00 |
Leonard Hall
|
2ab3d0b3b0
|
AC_AttitudeControl: Add Landed Gain Backoff
|
2024-07-25 09:50:35 +10:00 |
Leonard Hall
|
7047e11090
|
AC_AttitudeControl: Change input_quaternion to use body frame rates
|
2024-06-26 11:22:54 +10:00 |
Iampete1
|
f3c32a7c9e
|
AC_AttitudeControl: move `euler_rate_to_ang_vel`, `ang_vel_to_euler_rate` and `euler_accel_limit` to Quaternion attitude
|
2024-05-07 08:34:40 +09:00 |
Tatsuya Yamaguchi
|
26ec2ae952
|
AC_AttitudeControl: fix ATC_SLEW_YAW description (NFC)
|
2024-04-17 22:18:51 +10:00 |
Iampete1
|
6c4c7a2130
|
AC_AttitudeControl: fix reset_target_and_rate method
|
2024-02-19 09:15:58 +09:00 |
Mykhailo Kuznietsov
|
6c4d988631
|
AC_AttitudeControl: Fix some typos
Fixed some typos found in the code.
|
2023-10-12 18:30:42 +11:00 |
Andy Piper
|
31a2acb7ad
|
AC_AttitudeControl: rename get_angle_P_scale_logging()
|
2023-09-13 18:02:44 +10:00 |
Leonard Hall
|
ffc553f34f
|
AC_AttitudeControl: Fix yaw limit calculations
|
2023-09-12 19:14:01 +10:00 |
Peter Barker
|
f1eec8482b
|
AC_AttitudeControl: use quat.to_euler(Vector3f&)
|
2023-04-19 14:24:45 +10:00 |
Andy Piper
|
8ecd1d9a37
|
AC_AttitudeControl: move THR_G_BOOST to Multicopter only
refactor PD and Angle P boosting into update_throttle_gain_boost()
call update_throttle_gain_boost() from rate_controller_run()
|
2023-01-31 08:22:40 +09:00 |
Andy Piper
|
53b7f96a5d
|
AC_AttitudeControl: boost PD on roll and pitch when slew limit is hit
boost angle P when slew limit is hit
move to a single parameter for thrust-gain boosting
add PD scaling support
|
2023-01-11 18:59:52 +11:00 |
Leonard Hall
|
3c69d28237
|
AC_AttitudeControl: Support changing update period
|
2022-12-13 17:10:06 +11:00 |
Peter Barker
|
48d25cfc9f
|
AC_AttitudeControl: change namespace of MultiCopter and FixedWing params
this stops the libraries knowing anything about AP_Vehicle
|
2022-11-09 19:04:37 +11:00 |
Leonard Hall
|
aed694316d
|
AC_AttitudeControl: input_thrust_vector with general heading
|
2022-11-01 08:21:50 +09:00 |
Iampete1
|
14a786bdfa
|
AC_AttitudeControl: remove duplicate `_attitude_target.normalize()`
|
2022-10-18 08:30:46 +11:00 |
Andrew Tridgell
|
bd1be3b41c
|
AC_AttitudeControl: added single loop override of angle P gains
this is used by quadplanes in back-transiton to prevent oscillation
caused by driving the fixed wing controller too fast
|
2022-10-18 07:38:39 +11:00 |
Iampete1
|
07d96361ed
|
AC_AttitudeControl: params always use set method
|
2022-08-03 13:43:48 +01:00 |
Bill Geyer
|
2377d7a2c3
|
AC_AttitudeControl: move input_shaping_rate into input_shaping_ang_vel
|
2022-06-28 07:56:12 +09:00 |
Bill Geyer
|
be65358cc1
|
AC_AttitudeControl: incorporate suggested changes
|
2022-06-28 07:56:12 +09:00 |
Bill Geyer
|
fd24b3912f
|
AC_AttitudeControl: add comments
|
2022-06-28 07:56:12 +09:00 |
Bill Geyer
|
a547916ebf
|
AC_AttitudeControl: only use rate shaping tc if tc is nonzero
|
2022-06-28 07:56:12 +09:00 |
bnsgeyer
|
7594f7a558
|
AC_AttitudeControl: incorporate sqrt controller in rate shaping
|
2022-06-28 07:56:12 +09:00 |
Iampete1
|
ecc86b6a4b
|
AC_AttitudeControl: reduce alt hold min lean angle to 5deg on plane
|
2022-05-27 08:17:14 +10:00 |
murata
|
59dcf18558
|
AC_AttitudeControl: Shorten survival time of automatic variables
|
2022-05-16 09:08:02 +09:00 |
Leonard Hall
|
0d863aa736
|
AC_AttitudeControl: Allow diabling of slew limit
|
2022-05-14 22:31:43 +09:00 |
Andrew Tridgell
|
99a6cb69f8
|
AC_AttitudeControl: added get_rpy_srate()
and remove dmod binding, as slew rate turned out to be more useful
|
2022-05-03 10:01:19 +10:00 |
Andrew Tridgell
|
f8fe74f5fe
|
AC_AttitudeControl: added get_rpy_PDmod method
used for lua scripts to do VTOL tuning
|
2022-04-29 11:54:12 +10:00 |
Leonard Hall
|
b1f80fbe4f
|
AC_AttitudeControl: Remove double colon
|
2022-02-03 14:36:21 +09:00 |
Iampete1
|
b3646494d4
|
AC_AttitudeControl: always use smaller of slew yaw and rate max
|
2022-02-01 08:19:35 +09:00 |
Leonard Hall
|
1ad5479954
|
AC_AttitudeControl: use relax_integrator
|
2022-01-25 13:20:47 +09:00 |
Leonard Hall
|
7a9a0bfb3f
|
AC_AttitudeControl: Support MAVLINK_MSG_ID_SET_ATTITUDE_TARGET
|
2022-01-19 18:03:17 +11:00 |
Leonard Hall
|
0bdf34dc57
|
AC_AttitudeControl: Respect rate limit in max_rate_step
|
2022-01-11 10:57:53 +11:00 |
Andrew Tridgell
|
3f936baf5c
|
AC_AttitudeControl: adjust docs for rate max limits
after discussion with Leonard
|
2021-11-11 07:22:38 +11:00 |
Leonard Hall
|
ad278779e3
|
AC_AttitudeControl: : Add units to the accessors.
|
2021-09-09 08:01:14 +09:00 |
Iampete1
|
2a834508ae
|
AC_AttitudeControl: check for zero rate Y max before taking min
|
2021-08-25 23:48:52 +01:00 |
Leonard Hall
|
a32b5b3bb0
|
AC_AttitudeControl: Allow yaw rate reset to be de-selected
|
2021-07-13 09:51:36 +10:00 |
Peter Hall
|
716ceb93c5
|
AC_AttitudeControl: add thrust vector methods to 6DoF multi
|
2021-06-21 09:58:05 +09:00 |
Leonard Hall
|
359cf8ed0e
|
AC_AttitudeControl: Rename set_attitude_target_to_current_attitude
|
2021-05-26 16:03:05 +09:00 |
Leonard Hall
|
fb83f98b77
|
AC_AttitudeControl: Set rates to zero during arming procedure for acro
|
2021-05-26 16:03:05 +09:00 |
Leonard Hall
|
34e342f658
|
AC_AttitudeControl: Rename set_yaw_target_to_current_heading
|
2021-05-26 16:03:05 +09:00 |
Leonard Hall
|
b489dd5fe1
|
AC_AttitudeControl: Set yaw rate to zero during arming procedure
|
2021-05-26 16:03:05 +09:00 |
Leonard Hall
|
772cec5101
|
AC_AttitudeControl: minor format fix
|
2021-05-12 17:16:00 +10:00 |