Andrew Tridgell 8a03b3ba22 APM_Control: reduce elevator when past LIM_ROLL_CD ... this reduces elevator control when rolled over hard in fixed wing. Using the elevator when on the side just caused earth frame yaw and is counter productive. It can also prevent some aircraft from recovering from inverted flight.		2016-06-24 11:28:18 +10:00
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APM_Control.h	APM_Control: added a ground vehicle steering controller	2013-09-09 18:04:40 +10:00
AP_AutoTune.cpp	APM_Control: Fix typos	2016-05-13 19:20:05 -03:00
AP_AutoTune.h	APM_Control: replace header guard with pragma once	2016-03-16 18:40:41 +11:00
AP_PitchController.cpp	APM_Control: reduce elevator when past LIM_ROLL_CD	2016-06-24 11:28:18 +10:00
AP_PitchController.h	APM_Control: expose parameters as AP_Float	2016-05-07 18:34:06 +10:00
AP_RollController.cpp	APM_Control: raise default P and I gains, and set a lower limit on I for pitch	2016-03-25 09:54:53 +11:00
AP_RollController.h	APM_Control: expose parameters as AP_Float	2016-05-07 18:34:06 +10:00
AP_SteerController.cpp	APM_Control: Get steer rate using earth frame.	2016-06-01 10:05:20 +09:00
AP_SteerController.h	APM_Control: replace header guard with pragma once	2016-03-16 18:40:41 +11:00
AP_YawController.cpp	Global: rename min and max macros to uppercase	2015-12-01 16:28:09 -02:00
AP_YawController.h	APM_Control: remove unused _last_error member	2016-04-23 23:06:20 -07:00
TuningGuide.txt	APM_Control: Fix typos	2016-05-13 19:20:05 -03:00