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16,739 Commits 71 Branches 509 Tags 715 MiB
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70 Commits

Author SHA1 Message Date
Robert Lefebvre 23adf2773c AC_AttitudeControl: Remove To-Do comments for Attitude Rate logging. 2015-05-27 14:28:44 +10:00
Robert Lefebvre 915236f1f5 AC_AttitudeControl: Non-functional comment change 
Don't encourage future misuse of g.rc3
 2015-05-25 22:13:37 +09:00
Andrew Tridgell 326b0b33ea AC_AttitudeControl: revert AP_Math class change 2015-05-05 13:27:04 +10:00
Tom Pittenger 1bca81eaed AC_AttitudeControl: compiler warnings: apply is_zero(float) or is_equal(float) and float to doubles 2015-05-05 13:26:55 +10:00
Jonathan Challinger ab2532a609 AC_AttitudeControl: constrain _angle_boost to avoid overflow 2015-04-24 16:30:43 +09:00
Leonard Hall 24b8d32b0e AC_AttitudeControl: add comment 2015-04-16 21:00:22 +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 afcd1c6ec3 AC_AttitudeControl: sqrt controller on Stab 2015-04-09 20:19:43 +09:00
Jonathan Challinger e2383581cc AC_AttitudeControl: relax_bf_rate_controller resets rate integrators 2015-03-06 14:02:57 +09:00
Leonard Hall 20de383084 AC_AttControl: accel limiting for angular control only if feed forward enabled 2015-03-06 14:02:52 +09:00
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 eb084f7c58 AC_AttControl: bf yaw control uses input filtered PID 2015-03-06 14:02:21 +09:00
Jonathan Challinger 7224669399 AC_AttitudeControl: cleanup angle_ef_roll_pitch_rate_ef_yaw_smooth 2014-10-27 15:20:46 +09:00
Jonathan Challinger 0c4a489491 AC_AttitudeControl: use sqrt_controller function 2014-10-27 15:20:43 +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 f65e81cb07 AC_AttControl: remove some old comments 2014-10-04 23:49:21 +09:00
Randy Mackay 5a66ff1ef9 AC_AttControl: bug fix for ef target during acro 2014-08-23 22:17:54 +09:00
Randy Mackay 3e0b573dfe AC_AttControl: remove debug message 2014-08-22 22:58:48 +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 58257e3858 AC_AttControl: set rate D term filter from ins filter 2014-08-14 11:47:35 +09:00
lthall 329118b7c9 Copter: AC_ATT correct yaw error calculation 2014-08-14 11:47:13 +09:00
lthall 90dc9411a5 Copter: ACRO Error calculation fix 2014-08-14 11:47:08 +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
Randy Mackay eebd32f306 AC_AttControl: remove duplicate rate_ef_desired to resolve compiler warning 2014-07-16 21:50:31 +09:00
lthall fb55658c91 Copter: Acro use same error limit in all three axis 2014-07-16 17:46:13 +09:00
lthall 2889f5abc4 AC_AttControl: Fix feedforward behavior 2014-07-16 17:46:06 +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 0f7178e447 AC_AttControl: cast fabs to float to resolve compiler warning 2014-07-16 14:38:20 +09:00
Randy Mackay 971411e0db AC_AttControl: fixed typo in parameter description 2014-07-13 10:31:11 +09:00
Randy Mackay 46f25c52a4 AC_AttControl: allow enabling/disabling feedforward and accel limiting 2014-06-10 20:03:02 +09:00
Randy Mackay 130eb07d48 AC_AttControl: angle_ef_roll_pitch_rate_ef_yaw supports zero yaw accel 2014-06-10 20:02:58 +09:00
Randy Mackay b57c0dabf6 AC_AttControl: check accel_rp_max instead of rate_bff_ff_enabled 
We use the accel_rp_max, accel_y_max to check whether to apply accel
limiting or not.  This is related to separate from the
body-frame-feed-forward.
 2014-06-10 20:02:54 +09:00
Randy Mackay d9c966c927 AC_AttControl: RATE_FF_ENAB param to disable rate feed forward 2014-06-10 20:02:48 +09:00
Randy Mackay a662f87ffb AC_AttControl: remove resolved To-Do 
This To-Do is resolved by heli flight modes calling the
relax_bf_rate_controller method
 2014-06-10 20:02:45 +09:00
Randy Mackay 7f734f38d6 AC_AttControl: add earth frame angle constraints 
This should help recovery time if pilot switches out of ACRO (into
Stabilize, AltHold, etc) while inverted
 2014-06-10 20:02:43 +09:00
Randy Mackay 698cf934b8 AC_AttControl: formatting fixes 2014-06-10 20:02:42 +09:00
lthall 2bb63857fa AC_AttControl: clean up stabilize 2014-06-10 20:02:40 +09:00
lthall c24d293e1b AC_AttControl: zero _accel_xyz_max stops feed forward 
Also added place holder for turning off feed forward.
 2014-06-10 20:02:39 +09:00
lthall 922026c15c AC_AttControl: rate compensation for yaw 2014-06-10 20:02:34 +09:00
Randy Mackay 5209598459 AC_AttControl: rename init_targets to relax_bf_rate_controller 2014-06-10 20:02:27 +09:00
lthall 1bdde31f6b Copter: Fix zero throttle flip issue Stabilize 
The problem is that the init_targets is intended to ensure the
controller doesn't build up the I term when the throttle is low. Because
it is poorly named (or used) it have been written to do something else.
Here I change it to do what the code is trying to use it to do.
 2014-06-10 20:02:01 +09:00
Randy Mackay 0969e464fb AC_AttControl: set roll, pitch, yaw rate control D term filters 2014-05-29 17:40:17 +09:00
Randy Mackay 5876a2fe47 AC_AttControl: increase default rp accel to 900deg/s/s 2014-04-07 13:37:08 +09:00
Randy Mackay 7bff8e9312 AC_AttControl: constrain earth frame yaw angle error 
This temporarily resolves the wobble we see in Auto when the target
heading is suddenly changed leading to a large yaw angle error
 2014-03-29 20:42:21 +09:00
Randy Mackay 25ee5d5dc8 AC_AttControl: smoothing_gain to angle_ef_roll_pitch_rate_ef_yaw_smooth 
pair-programmed with lthall
 2014-03-04 22:23:14 +09:00
lthall 15f88c2a2b AC_AttControl: Stabilize input shaping 2014-03-04 21:52:18 +09:00