Modal synthesis of missle autopilot control law

미사일 자동 조종 제어 법칙의 형태합성

The purpose of this paper is to present an efficient and practical method for a Hissle autopilot design problem. The method emphasizes on the use of a modern design technique to classical flight control specifications and the trade-off between dynamic performance and robustness of the Missle autopilot control system.