Model following control for torque and rotor speed
Abstract:
A system and method for controlling a rotor of an aircraft is disclosed. A desired rotor speed for the rotor is received and a torque command that generates the received rotor speed is calculated. A fuel adjustment signal is calculated based on the torque command and a dynamic rotor measurement of the aircraft. The fuel adjustment signal is provided to the aircraft to track the rotor speed to the desired rotor speed.
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