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https://github.com/ArduPilot/ardupilot
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811e8571f1
this prevents a floating point error caused by using an uninitialised vector3 when switching between DCM and EKF control in AP_InertialNav Pair-Programmed-With: Randy Mackay <rmackay9@yahoo.com> |
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examples/AP_InertialNav_test | ||
AP_InertialNav_NavEKF.cpp | ||
AP_InertialNav_NavEKF.h | ||
AP_InertialNav.cpp | ||
AP_InertialNav.h |