To cope with threatens of fast development of high-speed and high maneuvering tactical ballistic missiles and other modern air weapons, intercept missiles are desired with capabilities of rapid and accurate response to hit to kill the targets. Since the traditional missiles with fins-only have a long response time and the effectiveness of fins severely depends on the surrounding environment, they can hardly kill the targets of high-speed and high maneuvering. By contrast, aero & reaction jets missile is effective on improving response speed, for the direct lateral force system composed of reaction jets responds fast and its effectiveness is independent with the surrounding environment. Thus, air defense missiles of the fourth generation mostly combine aerodynamic fins with director lateral force, and adopt blended control scheme. Research on the blended control of aero &reaction jets missiles is meaningful and worthy. Based on comprehensive analysis of aero & reaction jets missile features, several key problems of the blended control are deeply investigated. The main contributions are addressed as follows: (1). Motion equations of the missiles are derived. Model features of the aero & reaction jets missiles are comprehensively analyzed, indicating the properties of nonlinearity, time-scale separation, couplings from pitch and yaw channel, and couplings from aerodynamic fins and reaction jets. Particularly, control characteristics of the direct lateral force system are deeply analyzed. (2).As for coordination for fins and reaction jets, two coordination strategies are proposed. One is a modified control allocation strategy which takes account of the similarity of those two actuators in design. Another coordination strategy considering the different features of fins and reaction jets is proposed, in which the reaction jets control is first considered due to its inherent control error caused by their discrete trait, and then the aerodynamic fin control is designed based on the reaction jets control results. Those two coordination strategies are both verified by simulations. (3). To cope with system properties of nonlinearity, couplings, and huge disturbances and uncertainties, three robust attitude blended control schemes are proposed. The first is based on dynamic inversion compensated by fuzzy neural networks and dynamic control allocation; The second is using adaptive observer-based sliding mode control and fuzzy allocation; The last bases on generali...
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