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
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
d79403707b
AC_AttControl: add feed forward param descriptions
...
No functional change
2017-03-01 14:59:44 +09:00
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
189b766f2b
AC_AttControl: remove redundant parameter set
2017-01-17 14:56:07 +09:00
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
8419045aea
Spell in comments
2017-01-06 10:57:39 -08:00
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
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
2e2d39e628
AC_AttitudeControl: add missing parameter metadata
2016-10-27 09:15:03 -07:00
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
44830be172
AC_AttControl: add parameter check of throttle mix
2016-09-02 09:27:15 +09:00
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
8737f6b62d
AC_AttitudeControl: enhanced quaternion attitude controller
2016-06-24 17:17:11 +09:00
da946288a2
AC_AttitudeControl: rename throttle_ave_max to throttle_avg_max
2016-06-18 11:55:49 +09:00
570920c7d7
AC_AttitudeControlMulti: run control_monitor_update in rate_controller_run
2016-06-18 11:55:49 +09:00
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
dafc45eb26
AC_AttitudeControl: move get_althold_lean_angle_max to parent class
2016-06-18 11:55:49 +09:00
3d27ecca92
AC_AttitudeControl: add TC for Alt_Hold angle limit
2016-06-18 11:55:49 +09:00
7ff0fcb25d
AC_AttitudeControl: multicopter specific rate_controller_run
2016-06-18 11:55:49 +09:00
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
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
25c77c154f
AC_AttitudeControl: rename get_boosted_throttle to get_throttle_boosted
2016-06-18 11:55:49 +09:00
35ef761deb
AC_AttitudeControl: Move set_throttle_out to _Multi and _Heli
2016-06-18 11:55:49 +09:00
35c6ea994d
AC_AttControl_Multi: fix parameter descriptions
2016-04-01 11:59:30 +09:00
5edc16dfb4
AC_AttControl_Multi: add rate PIDs
2016-04-01 11:59:30 +09:00
6f29bbafb4
AC_AttControl_Multi: get_althold_lean_angle_max uses motor thrust in 0 to 1 range
2016-04-01 11:59:30 +09:00
24f975c16a
AC_AttControl_Multi: fix throttle boost for 0 to 1
2016-04-01 11:59:30 +09:00
bab08cbcc1
AC_AttControl_Multi: add divide by zero check
2016-04-01 11:59:30 +09:00
8c7f36563c
AC_AttControl: bug fix to angle_boost reporting
...
Thanks to OXINARF for finding this
2016-01-08 10:48:59 +09:00
5ddd332277
AC_AttControl: add ANGLE_BOOST param
...
This allows disabling angle boost
2016-01-07 12:31:52 +09:00
29ff5035b4
AC_AttControl: limit lean angle from throttle
2015-09-07 15:10:09 +09:00
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
bf2bf2e3fa
AC_AttControl_Multi: new multirotor specific attitude control class
2015-07-21 16:25:53 +09:00
Dr.-Ing. Amilcar Do Carmo Lucas
Randy Mackay
Andrew Tridgell
Leonard Hall
murata
Peter Barker
Mathieu OTHACEHE
Gustavo Jose de Sousa