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181 Commits

Author SHA1 Message Date
Leonard Hall ee82943f85 AC_AttitudeControl: add input_shaping_rate_predictor 2018-03-16 13:50:57 +09:00
Leonard Hall 6175a896ee AC_AttitudeControl: add set smoothing gain 
Smoothing gain value should be set once when entering a mode
 2018-03-16 13:50:57 +09:00
Leonard Hall 213f7a4061 AC_AttitudeControl: add get_accel_roll/pitch/yaw_max_radss methods 
Also constify existing get_accel_roll/pitch/yaw_max methods
 2018-03-16 13:50:57 +09:00
Leonard Hall 3ada0f32b0 AC_AttitudeControl: minor comment update 
Non-functional change
 2018-01-19 15:40:24 +09:00
Leonard Hall 75de0cb4ef AC_AttitudeControl: sqrt_controller accepts dt 2018-01-16 12:13:48 +09:00
Randy Mackay 6315e6eb45 AC_AttitudeControl: remove unused get_tilt_limit_rad 2017-11-15 20:22:02 +09:00
bnsgeyer e8173f27df AC_AttitudeControl: reset target attitude 
added method to reset current vehicle attitude to support swash
behaviors in Trad Heli
 2017-10-28 12:31:06 +11:00
Andrew Tridgell f2efea4e1d AC_AttitudeControl: added inverted flight support 
for helis
 2017-10-03 10:16:41 +11:00
Leonard Hall ed0063d10d AC_AttControl: save accel max using shorter set_and_save 
no functional change
 2017-06-22 15:20:16 +09:00
Leonard Hall 0544cf1d82 AC_AttControl: add step input for autotune 2017-06-22 15:18:04 +09:00
Andrew Tridgell fe3e7e8153 AC_AttitudeControl: added get_throttle_mix() 
and when we use set_throttle_mix_value(), set both desired and actual

thanks to Leonard for the suggestions
 2017-04-19 09:08:43 +10:00
Randy Mackay 67097c8d59 AC_AttitudeControl: use gyro_latest 
This allows moving the attitude control before the ahrs/ekf update

We continue to use ahrs.get_gyro for the non-time-critical heli
passthrough functions.  We should avoid using get_gyro_latest() unless we know there is a direct benefit because it could lead to inconsistent gyro values vs what the EKF is using.
 2017-03-03 13:14:28 +11:00
Andrew Tridgell e5ed20d6f7 AC_AttitudeControl: added set_throttle_mix_value() 
used by quadplane
 2017-02-26 09:20:51 +11:00
Andrew Tridgell 1345bf8737 AC_AttitudeControl: added support for AP_AHRS_View 
this allows for tailsitters with a different attitude view
 2017-02-18 17:26:43 +11:00
Leonard Hall c6d2fc3d5d AC_AttitudeControl: add rpy mix manual 
This allows adjusting the attitude control vs throttle level in manual
flight modes (Stabilize, ACRO)
 2017-01-17 14:19:09 +09:00
Andrew Tridgell 5cf1c0869d AC_AttitudeControl: expose all functions via abstract class 
this allows for a single class to be used for heli and multicopter
 2017-01-12 17:39:37 +11:00
Dr.-Ing. Amilcar Do Carmo Lucas 8419045aea Spell in comments 2017-01-06 10:57:39 -08:00
Mathieu OTHACEHE 152edf7189 Global: remove mode line from headers 
Using a global .dir-locals.el file is a better alternative than
reincluding the same emacs header in every file of the project.
 2016-10-24 09:42:01 -02:00
Tom Pittenger 3adf8c3e51 AC_AttitudeControl: comment odd math in get_att_target_euler_cd 
degree(100) = 1 float multiplicaiton
vector3f * degree(100.0f)  = 4 float multiplications
degree(vector3f) * 100.0f  = 6 float multiplications and needs new degree(vector3f) function
degree(vector3f * 100.0f)  = 6 float multiplications and needs new degree(vector3f) function

These all come to the same conclusion but the one that is faster appears to be a bug but is mathematically correct.
 2016-09-27 17:04:53 -07:00
Randy Mackay 44830be172 AC_AttControl: add parameter check of throttle mix 2016-09-02 09:27:15 +09:00
Randy Mackay 535158e0d8 AC_AttControl: move var_info declaration 
No functional change
 2016-09-02 09:27:12 +09:00
Leonard Hall 50b694444b AC_AttControl: correct method comments 
No functional change
 2016-08-08 11:24:42 +09:00
Leonard Hall ac04fcd836 AC_AttControl: fix set_yaw_target_to_current_heading 2016-08-05 12:40:37 +09:00
Leonard Hall 011bc0a350 AC_AttControl: add reset_rate_controller_I_terms() 2016-08-05 12:40:37 +09:00
Randy Mackay d5c18dc987 AC_AttControl: remove unused 100hz definition 2016-08-01 17:21:04 +09:00
Leonard Hall 8737f6b62d AC_AttitudeControl: enhanced quaternion attitude controller 2016-06-24 17:17:11 +09:00
Leonard Hall 117ae89505 AC_AttitudeControl: increase SLEW_YAW default to 60deg/sec 2016-06-24 16:24:17 +09:00
Randy Mackay 558f29b95c AC_AttitudeControl: control mixing made protected 2016-06-18 11:55:49 +09:00
Leonard Hall 096bdd67f8 AC_AttitudeControl: add ATC_ANG_LIM_TC parameter 
This allow adjusting the reponse to limit lean angles to reduce altitude loss
 2016-06-18 11:55:49 +09:00
Randy Mackay dafc45eb26 AC_AttitudeControl: move get_althold_lean_angle_max to parent class 2016-06-18 11:55:49 +09:00
Leonard Hall 3d27ecca92 AC_AttitudeControl: add TC for Alt_Hold angle limit 2016-06-18 11:55:49 +09:00
Randy Mackay 7ff0fcb25d AC_AttitudeControl: multicopter specific rate_controller_run 2016-06-18 11:55:49 +09:00
Leonard Hall 1fb4c12cd0 AC_AttitudeControl: move in throttle vs attitude prioritisation 
Previously this prioritisation of throttle vs attitude was done in the
AP_Motors library
 2016-06-18 11:55:49 +09:00
Randy Mackay 0870ce9fc1 AC_AttitudeControl: remove get_throttle_boosted from parent class 
This is only called from multicopters
 2016-06-18 11:55:49 +09:00
Leonard Hall 25c77c154f AC_AttitudeControl: rename get_boosted_throttle to get_throttle_boosted 2016-06-18 11:55:49 +09:00
Leonard Hall 35ef761deb AC_AttitudeControl: Move set_throttle_out to _Multi and _Heli 2016-06-18 11:55:49 +09:00
Andrew Tridgell e070aeebe3 AC_AttitudeControl: added accessors for P and D RMS controller values 2016-06-10 17:48:31 +10:00
Andrew Tridgell 1c463e3f3b AC_AttitudeControl: log rms P and D separately 
as discussed with Leonard
 2016-06-10 17:48:31 +10:00
Andrew Tridgell b4bdfa2451 AC_AttitudeControl: return roll, pitch and yaw controller error separately 
as discussed with Leonard
 2016-06-01 17:18:58 +10:00
Andrew Tridgell 6330060e49 AC_AttitudeControl: added monitoring of controller error 
use RMS P+I+FF output. Thanks to Leonard for the suggestion
 2016-05-28 17:33:30 +10:00
Andrew Tridgell c7664291f9 AC_AttitudeControl: fixed comment on function 2016-04-28 17:46:58 +10:00
Randy Mackay 75042e5e27 AC_AttControl: remove rate PIDs 2016-04-01 11:59:30 +09:00
Randy Mackay 17c9db08f3 AC_AttControl: add angle and rate PIDs 2016-04-01 11:59:30 +09:00
Randy Mackay c5e5b4f783 AC_AttControl: fix rate controller max definitions to -1 to +1 range 2016-04-01 11:59:30 +09:00
Leonard Hall 2822b93cd4 AC_AttControl: add get_throttle_in accessor 
Used for logging only
 2016-04-01 11:59:30 +09:00
Leonard Hall c0f209fa42 AC_AttControl: angle_boost to float 2016-04-01 11:59:30 +09:00
Lucas De Marchi f42484bcc5 AC_AttitudeControl: replace header guard with pragma once 2016-03-16 18:40:39 +11:00
Jonathan Challinger e946e047e6 AC_AttitudeControl: add attitude_controller_run functions, call from input functions 2016-03-02 20:16:18 +09:00
Leonard Hall 49a4bde5d9 AC_AttControl: lower minimum accelerations for large copters 2016-02-18 20:49:13 +09:00
Randy Mackay 5ddd332277 AC_AttControl: add ANGLE_BOOST param 
This allows disabling angle boost
 2016-01-07 12:31:52 +09:00
Jonathan Challinger 3d4bd92b48 AC_AttitudeControl: add helper functions to retrieve rotation matrices 2015-12-23 11:38:12 +09:00
Randy Mackay c8661f804f AC_AttControl: reduce compiler warnings by fixing member init order 
Also increased _dt's default to 400hz (no functional change)
 2015-12-09 20:04:42 +09:00
Randy Mackay 02eda4dcab AC_AttControl: remove comment, fix formatting 2015-12-09 20:04:32 +09:00
Jonathan Challinger e8345fbaab AC_AttitudeControl: rename getters for attitude target and attitude error 2015-12-09 19:58:48 +09:00
Jonathan Challinger 3a06edcee3 AC_AttitudeControl: rename local variable to match naming convention 2015-12-09 19:58:46 +09:00
Jonathan Challinger 162d2a9112 AC_AttitudeControl: naming changes in response to Leonard's review 2015-12-09 19:58:42 +09:00
Jonathan Challinger a48f201a04 AC_AttitudeControl: comment changes in response to Paul's review 2015-12-09 19:58:41 +09:00
Jonathan Challinger 0baf86c485 AC_AttitudeControl: fixup more names 2015-12-09 19:58:39 +09:00
Jonathan Challinger 41e580e53a AC_AttitudeControl: add input_att_quat_bf_ang_vel and use for ACRO 2015-12-09 19:58:38 +09:00
Jonathan Challinger 5919e95635 AC_AttitudeControl: add input_ prefix to input shaper functions 2015-12-09 19:58:36 +09:00
Jonathan Challinger bba360ea2b AC_AttitudeControl: correct bugs found in review 2015-12-09 19:58:35 +09:00
Jonathan Challinger 9208003aab AC_AttitudeControl: remove unused variable 2015-12-09 19:58:34 +09:00
Jonathan Challinger 1afab89991 AC_AttitudeControl: extensive renaming and recommenting 2015-12-09 19:58:29 +09:00
Jonathan Challinger 06c8457efd AC_AttitudeControl: rename and modify frame_conversion functions to follow conventions 2015-12-09 19:58:27 +09:00
Jonathan Challinger 7330de86e5 AC_AttitudeControl: change internals to use radians instead of centidegrees 2015-12-09 19:58:26 +09:00
Andrew Tridgell d8ee9feaac AC_AttitudeControl: fixed external tail gyro with no flybar 
this sets up the tail pass-through for acro mode
 2015-11-27 15:24:41 +09:00
Robert Lefebvre 0b33ef3862 AC_AttitudeControl: Add Hover Roll Trim functionality for helicopters. 2015-11-12 19:37:26 +09:00
Leonard Hall c8872e082d AC_AttControl: rename set_throttle_out parameter 
No functional change
 2015-09-07 15:10:15 +09:00
Leonard Hall 29ff5035b4 AC_AttControl: limit lean angle from throttle 2015-09-07 15:10:09 +09:00
Gustavo Jose de Sousa d49f10d2e5 AC_AttitudeControl: standardize inclusion of libaries headers 
This commit changes the way libraries headers are included in source files:

 - If the header is in the same directory the source belongs to, so the
 notation '#include ""' is used with the path relative to the directory
 containing the source.

 - If the header is outside the directory containing the source, then we use
 the notation '#include <>' with the path relative to libraries folder.

Some of the advantages of such approach:

 - Only one search path for libraries headers.

 - OSs like Windows may have a better lookup time.
 2015-08-11 16:28:41 +10:00
Randy Mackay 93dd7dd970 AC_AttControl: get_boosted_throttle purely virtual 2015-07-21 16:25:50 +09:00
Randy Mackay 1e3e65e443 AC_AttControl: add shift_ef_yaw_target 
This allows shifting the target heading in case the EKF shifts it's
heading estimate
 2015-06-24 11:49:32 +09:00
Leonard Hall cfc388934b AC_AttControl: add set_accel_roll_max 
Also equivalents for pitch and yaw
 2015-06-18 23:06:33 +09:00
Randy Mackay 7951346d72 AC_AttControl: bf_feedfoward_save made more concise 2015-05-08 14:29:49 +09:00
Leonard Hall cf45a1cf3a AC_AttitudeControl: add get accel and save ff 2015-05-08 14:14:30 +09:00
Leonard Hall 1900cc7582 AC_AttitudeControl: Enable FF by default 2015-05-08 14:14:21 +09:00
Jonathan Challinger b7f7624aac AC_AttitudeControl: add throttle filter cutoff parameter to set_throttle_out functions 2015-04-16 21:00:04 +09:00
Jonathan Challinger 518e798f53 AC_AttitudeControl: rework angle_boost 2015-04-16 20:59:58 +09:00
Jonathan Challinger f3555d0d43 AC_AttitudeControl: modify throttle interface to specify stabilization 2015-04-16 20:59:45 +09:00
Jonathan Challinger 5c2341009a AC_AttitudeControl: throttle is a float 2015-04-16 20:59:42 +09:00
Leonard Hall 4d9da2720b AC_AttitudeControl: add get for angle bf errors 2015-04-16 13:29:52 +09:00
Leonard Hall afcd1c6ec3 AC_AttitudeControl: sqrt controller on Stab 2015-04-09 20:19:43 +09:00
Leonard Hall 09aa2f8114 AC_AttitudeControl: Fix function discription 2015-03-23 07:40:04 -07:00
Leonard Hall 6b104c0529 AC_AttitudeControl: No Overshoot limit for Stab 
This maybe done in a more obvious way using a switch rather than just
making the overshoot larger than 180 degrees.
 2015-03-23 07:40:02 -07:00
Leonard Hall 792b2a2eb3 AC_AttControl: separate accel max for roll, pitch, yaw 
Also add:
Rate filters
rename rate filter defines
d-term only filter for roll, pitch rate control
accessors to save max accel for roll, pitch, yaw
fix for duplicate ACCEL_Y_MAX param
 2015-03-06 14:02:33 +09:00
Leonard Hall 9833c91b2b AC_AttControl: get_max_rate_step_bf_roll, pitch and yaw 2015-03-06 14:02:30 +09:00
Leonard Hall f00025e5c9 AC_AttControl: accessor for rate feedforward 2015-03-06 14:02:27 +09:00
Leonard Hall 691fb8947e AC_AttControl: accessor for rate_bf_targets 2015-03-06 14:02:25 +09:00
Leonard Hall 784a4ce51a AC_AttControl: increase max angle overshoot to 30deg 2015-03-06 14:02:23 +09:00
Robert Lefebvre 743c5e4fde AC_AttitudeControl: Remove un-needed #include 2015-01-21 14:36:54 +09:00
Randy Mackay 98f5a93e10 AC_AttControl: remove unused logging structure 2014-11-08 10:17:32 +09:00
Randy Mackay fc898a00a3 AC_AttControl: add sqrt_controller 
Original code by Jonathan Challinger
 2014-10-27 15:20:40 +09:00
Randy Mackay c45338f080 AC_AttControl: div-by-zero check for bf-to-ef conversion 2014-08-22 22:56:15 +09:00
Randy Mackay c2f8571f37 AC_AttControl: FF and accel limiting off by default 
Also adjust parameter ranges used by GCSs
 2014-07-17 16:22:32 +09:00
lthall fb55658c91 Copter: Acro use same error limit in all three axis 2014-07-16 17:46:13 +09:00
Randy Mackay 581838b271 AC_AttControl: initialise _acro_angle_switch 
Resolves a compiler warning
 2014-07-16 15:11:12 +09:00
Randy Mackay 83a84c7b90 AC_AttControl: add empty virtual destructor 
This resolves pixhawk bricking and reduces one compiler warning
 2014-07-16 14:56:52 +09:00
Jonathan Challinger 6e66cf43cb AC_AttitudeControl: Use bias-corrected angular rates instead of raw gyro measurements 2014-07-16 14:40:56 +09:00
Randy Mackay 5f623ac859 AC_AttControl: re-enable rate feedforward by default 
Roll and Pitch rate controllers became sluggish without feed-forward
enabled.
 2014-07-11 15:31:00 +09:00
Randy Mackay 46f25c52a4 AC_AttControl: allow enabling/disabling feedforward and accel limiting 2014-06-10 20:03:02 +09:00