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
Leonard Hall
e253c94f63
AC_AttitudeControl: Remove Unused Function
2021-04-27 17:13:55 +09:00
Leonard Hall
1fb2a95486
AC_AttitudeController: Thrust Vector attitude control
2021-04-27 17:13:55 +09:00
Peter Barker
a3c329b182
AC_AttitudeControl: make parameter renames consistent
2021-04-21 12:17:42 +10:00
Leonard Hall
b43c7f4ed1
AC_AttitudeControl: Parameter rename (non-functional)
2021-04-21 12:17:42 +10:00
hs293go
de0c57de77
AC_AttitudeControl: Use Quaternion::operator* for vector rotation
...
Replace all instances of the q*v*q.formula() or conversion to rotation
matrix + matrix multiply by calling Quaternion::operator* on a
vector
2021-04-21 12:17:42 +10:00
Leonard Hall
86a157ce59
AC_AttitudeControl: Seperate thrust vector correction into a separate function
2021-04-21 12:17:42 +10:00
Leonard Hall
c28d103afe
AC_AttitudeControl: Fix Angular velocity rotation to body frame
...
Thanks to BreederBai for higlighting this in issue #17059
Thanks to esaldiran and Hs293Go for helping check the math.
2021-04-19 14:48:59 +10:00
Randy Mackay
ae66803148
AC_AttitudeControl: minor optimisation and comment fixes
2021-04-03 12:07:59 +09:00
Leonard Hall
d6e3495eca
AC_AttitudeControl: support for feedforward rate in angle request for yaw
2021-04-03 12:07:59 +09:00
Leonard Hall
e788d63686
AC_AttitudeControl: clear up comment for inertial_frame_reset
2021-02-17 21:19:18 +09:00
Leonard Hall
f53242b323
AC_AttitudeControl: rename thrust_heading_rotation_angles args
2021-02-10 18:35:58 +11:00
Leonard Hall
ad6e2eeed8
AC_AttitudeControl: remove feed-forward from run_quat
2021-02-10 18:35:58 +11:00
Iampete1
7d5e5f8dd7
AC_AttitudeControl: add SITL panic to remind us to implent the quarternion
2021-02-09 12:43:54 +09:00
Leonard Hall
25fff17e48
AC_AttitudeControl: constify some local variables
2021-01-22 14:22:18 +09:00
Leonard Hall
1129a3fd59
AC_AttitudeControl: use AP_Math control functions
2021-01-20 18:19:40 +11:00
bnsgeyer
04e2cceaff
AC_AttitudeControl: Tradheli support for integrator management and hover collective learning
2020-12-21 23:33:48 -05:00
Mark Whitehorn
cc2c631d23
AC_AttitudeControl: add AC_AttitudeControl_TS
...
move tailsitter body-frame roll input method to new subclass
override relax_attitude_controllers in AttitudeControl_TS
2020-12-21 12:56:24 +11:00
Leonard Hall
edadbae240
AC_AttitudeControl: Handle zero accel value correctly in angle correction.
2020-06-23 08:21:47 +09:00
Randy Mackay
aff854f485
AC_AttitudeControl: update param ranges
2020-02-26 08:02:27 +09:00
Mark Whitehorn
7e8aecac50
AC_AttitudeControl: simplify body-frame roll axis swapping
2019-12-18 08:33:29 +11:00
Mark Whitehorn
bb9b116574
AC_AttitudeControl: fix argument order in tailsitter bodyframe roll input methods
...
increase allowed yaw error in tailsitter bodyframe roll modes
add combined bodyframe roll method
delete old versions of body-frame roll input methods
invert mc_controls
2019-12-18 08:33:29 +11:00
Leonard Hall
5afb5b4956
AC_AttitudeControl: Prevent loss of yaw control during large angle recovery.
2019-10-31 11:53:27 +08:00
Leonard Hall
0834726b48
AC_AttitudeControl: Support System ID tests
2019-10-16 08:17:09 +09:00
Leonard Hall
bbe33e38f3
AC_AttitudeControl: support for upgrade to PID object
2019-07-25 17:38:15 +09:00
