A method for controlling an aircraft includes receiving, via a processor of the aircraft, one or more signals indicative of a target attitude and a current attitude of the aircraft, determining, via the processor, an error in attitude based on comparing the target attitude and the current attitude, and generating, via the processor, a command signal for at least one propulsion unit of the aircraft based at least in part on the error in attitude and a feedback loop with angular acceleration feedback.
AIRCRAFT ATTITUDE CONTROL METHODS
2021-06-24
Patent
Elektronische Ressource
Englisch