A system for flight control system using simulator data for an electric aircraft is presented. The system includes a computing device, the computing device configured to receive a plurality of measured flight data, simulate a plurality of aircraft performance model outputs as a function of a flight simulator and the plurality of measured flight data, determine a moment datum as a function of the plurality of measured flight data and the plurality of aircraft performance model outputs, generate an allocation command datum as a function of the moment datum and the plurality of aircraft performance model outputs, and perform a torque allocation on a flight component of a plurality of flight components as a function of the allocation command and the moment datum.
SYSTEMS AND METHODS FOR FLIGHT CONTROL SYSTEM USING SIMULATOR DATA
2023-03-16
Patent
Electronic Resource
English
Dynamic Flight Simulator Control System
NTIS | 1988
|Springer Verlag | 2018
|Flight control system design for an in-flight simulator
AIAA | 1989
|