제어로봇시스템학회:학술대회논문집
- 1991.10a
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- Pages.355-360
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- 1991
A study on the gain-scheduling of missile autopilot
유도탄 제어기의 이득-스케듈링에 관한 연구
Abstract
A method of autopilot gain-scheduling is presented for missiles which have heavy aerodynamic coupling between pitch and yaw channels due to high maneuverability. Pitch and yaw, autopilot are cross-coupled, and their feedback gains are scheduled by total acceleration and bank angle for given Mach number and height. Bank angle information is obtained by using a simple estimator. By computer simulation, it is shown that the proposed method is superior to other existing methods.
Keywords