파라미터 최적화기법을 이용한 항공기 제어설계 자동화

Abstract

Automated controller parameter extraction technique for an classical-type controller is presented in this paper. Control design problem is formulated as parameter optimization problem, and optimal solutions are calculated by parameter optimization solver, hybridization of evolutionary programming and sequential quadratic programming. We applied this technique to a phase lead/lag compensator design and an aircraft flight control design problem, and obtained controller parameters satisfying design specifications.