Bounded Differential Game Guidance Law for Interceptor Missiles with Aero Fins and Reaction Jets
作者： Yunqian LI , Naiming QI , Wenhui ZHANG , Xianlu WANG
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摘要: A differential game guidance law for an endoatmospheric interceptor missile steered by aero fins and reaction jets is developed in this paper with bounded controls. For a low-altitude interceptor, the propellant of reaction-jet control system (RCS) restricted configuration. Considering limits, effect RCS thrust on homing performance investigated through space structures. Also, to use at appropriate timing, decomposition used determine initiating time RCS. Finally, effectiveness demonstrated realistic ballistic defense scenario. It shown that proposed provides significant improvement accuracy compared conditional one. Furthermore, under bigger cannot guarantee higher accuracy.
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