Pieterras Posted May 21, 2021 Posted May 21, 2021 Hi Team, The current implementation of the CCS is incorrect. When controlling pitch with the trim in CCS the attitude of the aircraft should be controlled, without adjusting the trimmed state of the aircraft. The aircraft should resume o normal 1G flight logic when disengaging the mode. Currently, when disengaging CCS, the aircraft pitch will not go back to normal logic, but seems to be trimmed out of normal logic. 1 1
Recommended Posts