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Lyapunov-based switched-gain impact angle control guidance 被引量:4
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作者 Zhongtao CHENG Lei LIU Yongji WANG 《Chinese Journal of Aeronautics》 SCIE EI CAS CSCD 2018年第4期765-775,共11页
To hit stationary ground targets in specified direction, a nonlinear impact angle control guidance law based on Lyapunov stability theory is proposed. The proposed law ensures the convergence of the heading angle and ... To hit stationary ground targets in specified direction, a nonlinear impact angle control guidance law based on Lyapunov stability theory is proposed. The proposed law ensures the convergence of the heading angle and the miss distance to guarantee a successful engagement. The impact angle can be adjusted by varying a single parameter. And the maximum value of acceleration has been analyzed to get the proper range for control parameter. Considering the achievable impact angle set is limited, an additional phase is added to form a two-phase control strategy.The first phase is to establish a proper initial condition for the second phase, and the second phase is to hit the target with a certain impact angle. An analysis of the proper selection of control parameters to expand the achievable impact angle set is presented. The performance of the proposed guidance law is illustrated with simulations. 展开更多
关键词 Composite achievable range GUIDANCE Impact angle control Lyapunov stability theory
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