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FEEDFORWARD AND FEEDBACK ADAPTIVE CONTROLLER FOR ROLLING CHANNEL OF AIR-TO-AIR MISSILE WITH MULTI-INPUT AND DISTURBANCES

On Yangling(Northweatern Polytechnical University)  
The parameters of midcourse air-air missile is very widely and significantly.It is diffcult to satisfy performance specifications for different altitudes trajetories using pure classical controller. However, to maintain good performance over a wide range of the altitudes and speeds of the missile,digital adaptive control methods may prove suitable.Adaptive flight control system schemes based on hyperstability theory are presented in this paper, the new schemes performance is superior to that without adaptive controller.
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