Modern Aircraft Model Description for Flight Control Law Design Challenge

초록

Modern aircraft requires not only the high level performance but also the robustness against the uncertainty. Since the classical control theory is insuficient for the purpose, the flight control system should be designed using modern control theory. It is important to examine which control theory is adequate for flight control system. This paper describes the benchmark aircraft model including the nonlinear dynamic model, the actuator model and environment model. Also, the linearized model about the trim point is drived for control law design. User-friendly computer aided toll is developed for evaluation.