mirror of https://github.com/ArduPilot/ardupilot
037469db30
this prevents I term buildup in the XY velocity controller during landing. This to account for the EKF giving a non-zero horizontal velocity when we have touched down. The I term buildup in the XY velocity controller can lead to the attitude error going above the level for disabling the relax function as the throttle mix is changed. That results in large motor outputs which can tip over the vehicle after touchdown. Thanks to Leonard for the suggestion |
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.. | ||
AC_Circle.cpp | ||
AC_Circle.h | ||
AC_Loiter.cpp | ||
AC_Loiter.h | ||
AC_WPNav.cpp | ||
AC_WPNav.h | ||
keywords.txt |