Iampete1
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c1e4ed6512
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AC_AttitudeControl: check for zero rate Y max before taking min
|
2021-08-28 12:50:32 +10:00 |
Andrew Tridgell
|
128c21cba2
|
AC_AttitudeControl: this fixes an issue with Z accel initialisation
tailsitter quadplanes were climbing a lot on transition from fixed
wing to Q modes. Leonard tracked it down to a bug in the Z accel init
|
2021-08-16 15:05:24 +10:00 |
Andrew Tridgell
|
10574f5188
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AC_AttitudeControl: apply EKF Z gain scaler
for flying with DCM
|
2021-08-16 15:03:55 +10:00 |
Leonard Hall
|
62c4a34660
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AC_AttitudeControl: AC_PosControl: support Control: Refactor to use Jerk
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2021-08-14 16:41:52 +10:00 |
Leonard Hall
|
3f33ac0a82
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AC_AttitudeControl: Fix Angle Vel units on function
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2021-08-14 16:41:52 +10:00 |
Leonard Hall
|
0d52cd4aeb
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AC_AttitudeControl: AC_PosControl: fix PID filter names FILT -> FLTE, D_FILT -> FLTD
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2021-08-14 16:41:52 +10:00 |
Leonard Hall
|
628206b5e8
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AC_AttitudeControl: Support thrust to weight of 10:1
|
2021-08-14 16:41:52 +10:00 |
Leonard Hall
|
730ac9cb20
|
AC_PosControl: Add MAX(bla,0) because safe_sqrt isn't safe
|
2021-07-22 16:01:01 +10:00 |
Leonard Hall
|
3d6dd8cff8
|
AC_AttitudeControl: AC_PosControl: calculate cross track
|
2021-07-22 16:01:01 +10:00 |
Leonard Hall
|
2dea0fa966
|
AC_AttitudeControl: AC_PosControl: Auto Terain following update
|
2021-07-22 16:01:01 +10:00 |
Leonard Hall
|
902560953b
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AC_AttitudeControl: Allow yaw rate reset to be de-selected
|
2021-07-22 16:01:01 +10:00 |
Leonard Hall
|
fcca42410a
|
AC_AttitudeControl: Add accessor for yaw slew limit
|
2021-07-22 16:01:01 +10:00 |
Leonard Hall
|
c3c3a47e9a
|
AC_AttitudeControl: AC_PosControl: support accel only input in the vertical
|
2021-07-22 16:01:01 +10:00 |
Leonard Hall
|
ebd8401652
|
AC_AttitudeControl: AC_PosControl: support terrain following
|
2021-07-22 16:01:01 +10:00 |
Leonard Hall
|
c1484f4b31
|
AC_AttitudeControl: AC_PosControl: seperate kinimatic shaping from pid limit setting
|
2021-07-22 16:01:00 +10:00 |
Leonard Hall
|
9d8fdf3e85
|
AC_AttitudeControl: Add terain following to guided
|
2021-07-22 16:01:00 +10:00 |
Leonard Hall
|
d5d7e3d5d3
|
AC_AttitudeControl: AC_PosControl: Support Accel only input
|
2021-07-22 16:01:00 +10:00 |
Leonard Hall
|
a546a9ac14
|
AC_AttitudeControl: AC_PosControl: Change input_pos_xyz name
|
2021-07-22 16:01:00 +10:00 |
Leonard Hall
|
68b882d404
|
AC_AttitudeControl: Add shaping_tc_z_s accessor
|
2021-07-04 08:19:11 +10:00 |
Leonard Hall
|
83b4616a7b
|
AC_PosControl: fixup ekf reset
|
2021-07-04 08:19:11 +10:00 |
Andrew Tridgell
|
0af57de50c
|
AC_AttitudeControl: convert poscontrol to use double position
|
2021-07-04 08:19:11 +10:00 |
Andrew Tridgell
|
e191c48d9f
|
AC_AttitudeControl: cleanup poscontrol comments with input from Leonard
|
2021-07-04 08:19:11 +10:00 |
Andrew Tridgell
|
6bde607aaa
|
AC_AttitudeControl: fixed comment
|
2021-07-04 08:19:11 +10:00 |
Andrew Tridgell
|
a4220b1584
|
AC_AttitudeControl: cleanup position control APIs
use Vector2 for xy, float for z
|
2021-07-04 08:19:11 +10:00 |
Leonard Hall
|
ee9ae3e570
|
AC_AttitudeControl: AC_PosControl: Init and stopping point fixes
|
2021-07-04 08:19:10 +10:00 |
Leonard Hall
|
b73182db3c
|
AC_AttitudeControl: AC_PosControl: change force_descend to ignore_descent_limit
|
2021-07-04 08:19:10 +10:00 |
Leonard Hall
|
20158ddf5f
|
AC_AttitudeControl:AC_PosControl: vibration failsafe fix
|
2021-07-04 08:19:10 +10:00 |
Leonard Hall
|
ab8f3c21ec
|
AC_AttitudeControl: AC_PosControl: Remove extra accel limit
|
2021-07-04 08:19:10 +10:00 |
Peter Hall
|
5a1fdf9f78
|
AC_AttitudeControl: add thrust vector methods to 6DoF multi
|
2021-07-04 08:19:10 +10:00 |
Hwurzburg
|
27620322ec
|
AC_AttitudeControl: remove % as units on params that are unitless
|
2021-05-30 22:38:27 -07:00 |
Hwurzburg
|
3f4d4e45fc
|
AC_AttitudeControl: correct param ranges to accomodate TradHeli defaults
|
2021-05-28 09:44:11 +09:00 |
Randy Mackay
|
d9c68031fa
|
AC_PosControl: write_log checks xy and z controllers are active
This allows write_log to be write PSCZ messages for modes with onlyi vertical control (e.g. althold) without also logging out-of-date PSC messages
|
2021-05-26 18:58:31 +10:00 |
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 |
Hwurzburg
|
ff931c7490
|
AC_AttitudeControl: make centideg metadata incr and range consistent
|
2021-05-25 10:10:18 +10:00 |
Leonard Hall
|
491350c1d6
|
AC_AttitudeControl: Fix before squash
|
2021-05-24 20:13:37 +10:00 |
Andrew Tridgell
|
8213fc5277
|
AC_AttitudeControl: prevent panic on SITL when no lock-step scheduling
this disables the internal error for bad timing on SITL types without
lock-step scheduling, such as RealFlight
|
2021-05-24 20:13:37 +10:00 |
Leonard Hall
|
92e05e8c4f
|
AC_AttitudeControl: PosControl fixes
|
2021-05-24 20:13:37 +10:00 |
Leonard Hall
|
7f1f29c1ae
|
AC_PosControl: rename get_roll_cd get_pitch_cd
|
2021-05-12 17:16:00 +10:00 |
Leonard Hall
|
f24a0988f4
|
AC_PosControl: minor formatting fixes
|
2021-05-12 17:16:00 +10:00 |
Leonard Hall
|
772cec5101
|
AC_AttitudeControl: minor format fix
|
2021-05-12 17:16:00 +10:00 |
Leonard Hall
|
4158c37cfa
|
AC_PosControl: Calculate heading
|
2021-04-27 17:13:55 +09:00 |
Leonard Hall
|
e253c94f63
|
AC_AttitudeControl: Remove Unused Function
|
2021-04-27 17:13:55 +09:00 |
Leonard Hall
|
bb46f7a947
|
AC_PosControl: Thrust Vector output
|
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 |