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New three-dimensional guidance law for BTT missiles based on differential geometry and Lie-group 被引量:2
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作者 Shuangchun Peng Liang Pan Tianjiang Hu Lincheng Shen 《Journal of Systems Engineering and Electronics》 SCIE EI CSCD 2011年第4期684-690,共7页
A new non-decoupling three-dimensional guidance law is proposed for bank-to-turn (BTT) missiles with the motion coupling problem. In this method, the different geometry is taken for theoretically modeling on B-IT mi... A new non-decoupling three-dimensional guidance law is proposed for bank-to-turn (BTT) missiles with the motion coupling problem. In this method, the different geometry is taken for theoretically modeling on B-IT missiles' motion within the threedimensional style without information loss, and meanwhile, Liegroup is utilized to describe the line-of-sight (LOS) azimuth when the terminal angular constraints are considered. Under these cir- cumstances, a guidance kinematics model is established based on differential geometry. Then, corresponding to no terminal angular constraint and terminal angular constraints, guidance laws are re- spectively designed by using proportional control and generalized proportional-derivative (PD) control in SO(3) group. Eventually, simulation results validate that this developed method can effectively avoid the complexity of pure Lie-group method and the information loss of the traditional decoupling method as well. 展开更多
关键词 three-dimensional guidance law differential geometry Lie-group control bank-to-turn (BTT).
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