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64 Commits

Author SHA1 Message Date
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
Leonard Hall 35ef761deb AC_AttitudeControl: Move set_throttle_out to _Multi and _Heli 2016-06-18 11:55:49 +09:00
Andrew Tridgell 9bf0ada875 AC_AttitudeControl: removed use of AFF for tail control in heli 2016-05-12 17:37:22 +10:00
Francisco Ferreira b7135175c9 AC_AttitudeControl: fix heli documentation 2016-04-18 07:40:34 +09:00
Randy Mackay 165d739b45 AC_AttControl_Heli: roll, pitch, yaw passthrough to motors in -1 to +1 range 2016-04-01 11:59:30 +09:00
Randy Mackay 344d86a095 AC_AttControl_Heli: fix parameter description 2016-04-01 11:59:30 +09:00
Randy Mackay 685be4083c AC_AttControl_Heli: remove unnecessary cast to AC_HELI_PID 2016-04-01 11:59:30 +09:00
Randy Mackay 6c91e50f8c AC_AttControl_Heli: remove scaling for centi-degrees and legacy motor input 2016-04-01 11:59:30 +09:00
Randy Mackay 32d238187f AC_AttControl_Heli: get_althold_lean_angle_max in 0 to 1 range 2016-04-01 11:59:30 +09:00
Randy Mackay db04dddba5 AC_AttControl_Heli: adjust rate gain param descriptions 2016-04-01 11:59:30 +09:00
Randy Mackay 7f2c1f830f AC_AttControl_Heli: add rate PIDs 2016-04-01 11:59:30 +09:00
Randy Mackay 2b123ee15d AC_AttControlHeli: fix rate_bf_to_motor_roll_pitch and yaw output in -1 to +1 range 2016-04-01 11:59:30 +09:00
Leonard Hall e5d6d45851 AC_AttControl_Heli: angle_boost to float 2016-04-01 11:59:30 +09:00
dgrat 5148e41c1a AP_Math: Cleaned macro definitions 
Moved Definitions into a separate header. Replaced PI with M_PI and
removed the M_PI_*_F macros.
 2016-02-27 02:51:33 -03:00
Andrew Tridgell fbacb4c01f AC_AttitudeControl: fixed M_PI -> M_PI_F 2015-12-20 17:55:39 +11:00
Jonathan Challinger 162d2a9112 AC_AttitudeControl: naming changes in response to Leonard's review 2015-12-09 19:58:42 +09:00
Jonathan Challinger 0baf86c485 AC_AttitudeControl: fixup more names 2015-12-09 19:58:39 +09:00
Jonathan Challinger 5919e95635 AC_AttitudeControl: add input_ prefix to input shaper functions 2015-12-09 19:58:36 +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
Robert Lefebvre 62864c9e2b AC_AttitudeControl_Heli: Remove commented out Cyclic Cross-Coupling code. Will resurrect in future. 2015-11-12 19:37:19 +09:00
Robert Lefebvre b8ce23970d AC_AttitudeControl_Heli: Implement Pirouette Compensation 2015-11-12 19:37:18 +09:00
Lucas De Marchi 831d8acca5 Remove use of PROGMEM 
Now variables don't have to be declared with PROGMEM anymore, so remove
them. This was automated with:

    git grep -l -z PROGMEM | xargs -0 sed -i 's/ PROGMEM / /g'
    git grep -l -z PROGMEM | xargs -0 sed -i 's/PROGMEM//g'

The 2 commands were done so we don't leave behind spurious spaces.

AVR-specific places were not changed.
 2015-10-30 14:35:16 +09:00
Andrew Tridgell e3f7b002c2 AC_AttitudeControl: use non-flybar leaky I handling 
The standard leaky-I handling works fine on a flybar, so better not to
have a special case that isn't needed
 2015-09-25 12:05:43 +10:00
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
Andrew Tridgell eeb97800ae AC_AttitudeControl: allow for tail pass-thru in ACRO mode 
this allows for all channels to be passed through
 2015-06-26 12:45:38 +09:00
Robert Lefebvre 4da54783fd AC_AttitudeControl_Heli: Semantic Change. Motor Runup to Rotor Runup. 2015-05-29 17:46:23 +09:00
Andrew Tridgell 521dae1c65 AC_AttitudeControl: use set_desired_rate() on PID controllers 
this sets them up for logging of PIDs
 2015-05-27 14:28:49 +10:00
Robert Lefebvre 353879cd2b AC_AttitudeControl_Heli: Add Rate Accel FF to Yaw control 2015-05-27 14:28:47 +10:00
Tom Pittenger 4f1dd2c8a4 AC_AttitudeControl: compiler warning stuff 
float to double promotion via cos & sin instead of cosf & sinf
(this code is commented out but in case it ever gets included it would be nice to be correct
 2015-05-16 08:21:36 +10:00
Tom Pittenger 70bef20a29 AC_AttitudeControl: replace fabs() with fabsf() 2015-05-09 09:57:26 +10:00
Randy Mackay bef5633ed5 AC_AttControlHeli: use params from parent class 2015-05-08 14:50:36 +09:00
Jonathan Challinger 87500d9d70 AC_AttitudeControl: use new lowpass filter 2015-04-17 10:46:45 +09:00
Jonathan Challinger 518e798f53 AC_AttitudeControl: rework angle_boost 2015-04-16 20:59:58 +09:00
Randy Mackay bdfe8bbc54 AC_AttControl_Heli: remove RATE_RP_MAX, RATE_Y_MAX 2015-04-09 20:19:54 +09:00
Randy Mackay e4d48fdc92 AC_AttControlHeli: separate accel max for roll, pitch 
renamed _accel_y_max to _accel_yaw_max
 2015-03-06 14:02:36 +09:00
Leonard Hall 51455af51a AC_AttConHeli: integrate PID input filter 2015-03-06 14:02:35 +09:00
Randy Mackay 3e1bd04c94 TradHeli: update AttControl params to match multicopters 2014-09-09 14:41:57 +09:00
Randy Mackay f6e12bda06 AC_AttControlHeli: integrate div-by-zero check for bf-to-ef conversion 2014-08-22 22:56:18 +09:00
Randy Mackay 691a3d8126 AC_AttControlHeli: add passthrough_bf_roll_pitch_rate_yaw 2014-08-22 16:28:57 +09:00
Robert Lefebvre 9b1d9e3cf0 AC_AttitudeControl_Heli: Add passthrough_to_motor_roll_pitch function. 2014-08-22 16:28:42 +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 76507a9e67 AC_AttControlHeli: remove hal declaration to clear compiler warning 2014-07-16 14:38:32 +09:00
Randy Mackay 5128991a84 AC_AttControlHeli: cast fabs to float to resolve compiler warning 2014-07-16 14:38:29 +09:00
Robert Lefebvre a7f6a91827 AC_AttitudeControl_Heli: Remove ToDo. Rate controllers should always run even if throttle is zero. 2014-07-13 17:11:20 +09:00