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474 Commits

Author SHA1 Message Date
Andrew Tridgell f2efea4e1d AC_AttitudeControl: added inverted flight support 
for helis
 2017-10-03 10:16:41 +11:00
Andrew Tridgell 99aad41955 AC_AttitudeControl: added a update_vel_controller_xy() API 
this allows for just XY control of velocity for quadplanes
 2017-09-09 08:14:09 +10:00
Andrew Tridgell 1a25087dd5 AC_AttitudeControl: fixed PIRO_COMP index 
this is a new conflict due to stricter checking in AP_Param
 2017-08-14 09:28:57 +09:00
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
Peter Barker d56eca036d AC_AttitudeControl: correct parameter markup 2017-06-05 21:02:30 +10:00
Leonard Hall ad74769fb7 AC_AttControl: adjust default rate IMAX and Yaw Filt 
Increase Roll, Pitch and Yaw IMAX from 0.444 or 0.222 to 0.5
Decrease Yaw Filter from 5hz to 2.5hz based on the results of autotunes on many vehicles which always seems to produce values between 2 and 3hz
 2017-06-01 10:08:41 +09:00
Dr.-Ing. Amilcar Do Carmo Lucas 188dfb6936 AC_AttitudeControl: Use SI units conventions in parameter units 
Follow the rules from:
http://physics.nist.gov/cuu/Units/units.html
http://physics.nist.gov/cuu/Units/outside.html
and
http://physics.nist.gov/cuu/Units/checklist.html
one further constrain is that only printable (7bit) ASCII characters are allowed
 2017-05-17 18:07:25 +10:00
Randy Mackay 3a397584a1 AC_PosControl: z-axis stopping point up to 3m above vehicle 
Stopping point while descending remains at 2m for safety
 2017-04-28 09:10:02 +09:00
Leonard Hall 6e92f74ca0 AC_PosControl: add clear_desired_velocity_ff_z method 2017-04-28 09:10:02 +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 132979b12f AC_PosControl: protect against POS_Z_P, ACCEL_Z_P divide-by-zero 2017-03-15 09:22:23 +09:00
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
Randy Mackay d79403707b AC_AttControl: add feed forward param descriptions 
No functional change
 2017-03-01 14:59:44 +09:00
Andrew Tridgell e5ed20d6f7 AC_AttitudeControl: added set_throttle_mix_value() 
used by quadplane
 2017-02-26 09:20:51 +11:00
Jacob Walser 0e124d0be5 AC_PosControl: Add AC_PosControl_Sub class 2017-02-21 11:26:14 +11:00
Jacob Walser 925fa5d214 AC_AttitudeControl: Add AC_AttitudeControl_Sub class 2017-02-21 11:26:14 +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
Andrew Tridgell 5acbf5d16e AC_AttitudeControl: use FF from AC_PID 2017-02-18 17:26:43 +11:00
Randy Mackay ff042528fe AC_PosControl: remove alt_max 
AC_Avoidance enforces the altitude limit
 2017-01-18 09:35:47 +09:00
Randy Mackay 127404acea AC_PosControl: add get_pos_z_kP accessor 2017-01-18 09:35:47 +09:00
Randy Mackay 189b766f2b AC_AttControl: remove redundant parameter set 2017-01-17 14:56:07 +09:00
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
Pierre Kancir 421524951f AC_PosControl: remove unnecessary parentheses 2016-12-05 10:59:45 -08:00
murata bcdd836820 AC_AttControl: remove unnecessary check of thr-mix-min 
Checks directly above ensure this check can never be true
 2016-12-01 13:52:04 +09:00
Leonard Hall 8af192ed9d AC_AttControl: allow MOT_THR_MIX_MAX to be 2.0 
The parameter description maximum of 0.9 should keep most users from
setting this parameter above 0.9 but there are rare cases for very high powered copters with low hover-throttle values where setting as high as 2.0 improves attitude control
 2016-11-30 17:56:34 +09:00
Randy Mackay 1012333eef AC_PosControl: add ekf position reset handling 
Previously this was in AC_WPNav and used only for loiter but it should work for any flight modes that use horizontal or vertical position control
 2016-11-24 19:57:56 +09:00
Leonard Hall ea0e413b04 AC_AttControl: do not limit rate if ATC_ACCEL_MAX param is zero 2016-11-23 14:43:29 +09:00
Peter Barker 2e2d39e628 AC_AttitudeControl: add missing parameter metadata 2016-10-27 09:15:03 -07:00
Leonard Hall 42672de606 AC_PosControl: set Alt_Hold filter for PID not just D 
We normally don't use the D term here so setting the filter for PID not
just D lets us smooth the throttle response.
 2016-10-26 21:00:43 +09:00
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
Jonathan Challinger 5a8db4f271 AC_PosControl: add interface to override horizontal velocity process variable 2016-10-14 10:46:01 +09:00
Jonathan Challinger 77dbf99cee AC_PosControl: fix bug related to ekfNavVelGainScaler 2016-10-11 15:25:59 +09:00
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
Leonard Hall fdcdcb0033 AC_PosControl: check Z-axis accel imax can always overpower hover throttle 
This removes the possibility of the vehicle constantly climbing if the hover throttle becomes a very large value
 2016-09-05 14:19:43 +09:00
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 29d4790fc7 AC_AttControl: reduce max_rate_step based on hover throttle 
This changes reduces AutoTune's twitch size based on the hover throttle
This method is only used by AutoTune
 2016-08-12 22:29:53 +09:00
Leonard Hall 50b694444b AC_AttControl: correct method comments 
No functional change
 2016-08-08 11:24:42 +09:00
Leonard Hall 34055944cd AC_PosControl: fix relax_alt_hold_controllers 2016-08-05 12:40:37 +09:00
Randy Mackay 24044e5611 AC_AttControl: get_throttle_avg_max always returns value in 0 to 1 range 
throttle_avg_max is the total average throttle level (expressed as a number from 0 to 1) that the motors can safely be raised to in order to maintain attitude control.  This level can be higher than the pilot's or autopilot provided throttle level.
Previously passing in a negative throttle_in could result in a negative throttle_avg_max being returned.
 2016-08-05 12:40:37 +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
Jonathan Challinger 630e5378da AC_PosControl: add get_horizontal_error 2016-07-12 18:40:25 +09:00
Leonard Hall 80bda572ba AC_AttutudeControl: Yaw shift fix 2016-06-24 18:15:48 +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 a1548405c1 AC_AttitudeControlHeli: fix althold lean angle max 2016-06-24 15:03:59 +09:00
Andrew Tridgell d1b28aaed9 AC_AttitudeControl: fixed factor of 1000 error in init_takeoff 2016-06-22 11:48:43 +10:00
Randy Mackay ec7c1ab0b0 AC_PosControl: comment fix to set_alt_max method 
No functional change
 2016-06-18 11:55:49 +09:00
Leonard Hall dcbb071c07 AC_PosControl: Move hover throttle calculation to AP_Motors 2016-06-18 11:55:49 +09:00
Randy Mackay b27da7699e AC_AttitudeControlMulti: get_throttle_avg_max made private 
Also fixed up method's description
 2016-06-18 11:55:49 +09:00
Randy Mackay da946288a2 AC_AttitudeControl: rename throttle_ave_max to throttle_avg_max 2016-06-18 11:55:49 +09:00
Randy Mackay 570920c7d7 AC_AttitudeControlMulti: run control_monitor_update in rate_controller_run 2016-06-18 11:55:49 +09:00
Leonard Hall 1639e22b74 AC_AttitudeControl: set desired_vel for reporting purposes even when not used 2016-06-18 11:55:49 +09:00
Randy Mackay 558f29b95c AC_AttitudeControl: control mixing made protected 2016-06-18 11:55:49 +09:00
Leonard Hall 9bd8878c8b AC_AttitudeControlHeli: fix update_althold_lean_angle_max 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
Randy Mackay b7431b7d0c AC_AttitudeControl: update throttle rpy mix on every iteration 2016-06-18 11:55:49 +09:00
Leonard Hall ca2977decf AC_AttitudeControl: set throttle vs attitude priority for flipped state 
When performing a flip we want to allow throttle to go high to provide
maximum attitude control
 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
Tom Pittenger 64c2510be9 AC_AttitudeControl: fix compile warning float to double promotion in string conversion 2016-06-01 17:38:47 -07:00
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 9bf0ada875 AC_AttitudeControl: removed use of AFF for tail control in heli 2016-05-12 17:37:22 +10:00
dgrat 41661f815f AP_Math: Replace the pythagorous* functions with a variadic template 
The new function can deal with a variable number of function parameters.
Additionally, I renamed the functions to norm(), because this is the
standard name used in several other projects.
 2016-05-10 11:41:26 -03:00
Randy Mackay 4a06ca4be2 AC_AttControl: remove unused call to motors.set_stabilizing 
Also minor change to order of a call to motors library to make stabilizing
and non-stabilizing calls consistent.

Non functional change
 2016-05-07 10:08:38 +09:00
Andrew Tridgell c7664291f9 AC_AttitudeControl: fixed comment on function 2016-04-28 17:46:58 +10:00
Andrew Tridgell 23a64e1227 AC_AttitudeControl: fixed accel limit trigonometry 
Leonard had mentioned the limit should be tan(angle) not sin(angle). I
noticed this one was wrong.
 2016-04-28 16:15:15 +10:00
Francisco Ferreira b7135175c9 AC_AttitudeControl: fix heli documentation 2016-04-18 07:40:34 +09:00
Andrew Tridgell d03a232659 AC_AttitudeControl: added set_limit_accel_xy() API 
for preventing integrator buildup
 2016-04-10 22:01:18 +10:00
Randy Mackay 87399776a3 AC_PosControl: hover throttle default to 0.5 2016-04-01 11:59:30 +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 35c6ea994d AC_AttControl_Multi: fix parameter descriptions 2016-04-01 11:59:30 +09:00
Randy Mackay ace58d114f AC_AttControl_Multi: reduce rate gain defaults 2016-04-01 11:59:30 +09:00
Leonard Hall b30606bb22 AC_AttControl: remove scaling for centi-degrees and legacy motor input 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 5edc16dfb4 AC_AttControl_Multi: add rate PIDs 2016-04-01 11:59:30 +09:00
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 c49a914597 AC_AttControlHeli: remove unnecessary virtual declaration 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
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 979534279a AC_AttControl: roll, pitch, yaw output to motors in -1 to +1 range 2016-04-01 11:59:30 +09:00