Systems and methods for flight control on an electric aircraft. The system includes a propulsor configured to generate lift to propel an electric aircraft, a pilot input mechanically coupled to the electric aircraft, a sensor communicatively connected to the pilot input, and a flight controller communicatively connected to the sensor. Sensor is configured to detect an input datum from the pilot input and convert the input datum into a command datum for the propulsor as a function of input mapping. Input mapping is determined as a function of the phase of flight.
SYSTEMS AND METHODS FOR FLIGHT CONTROL FOR AN ELECTRIC AIRCRAFT
2024-02-22
Patent
Electronic Resource
English
IPC: | B64C AEROPLANES , Flugzeuge |
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