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一种新的变结构制导律研究
引用本文:王广宇. 一种新的变结构制导律研究[J]. 航天控制, 2005, 23(3): 14-19
作者姓名:王广宇
作者单位:装备指挥技术学院,北京,101416
摘    要:在非线性相对运动学基础上提出了一种新的变结构制导律。变结构制导律仅利用了目标加速度界限的信息,因而在拦截过程中,并不需要精确的测量目标加速度,也就是取得了对目标机动的鲁棒性。在执行上,变结构制导律仅使用了视线转率测量值,因而和比例导引同样简单。仿真结果表明,所提出的制导律与比例导引相比有较大的性能改善。

关 键 词:非线性相对运动学  鲁棒性  变结构控制  制导律
文章编号:1006-3242(2005)03-0014-06
修稿时间:2004-09-01

Study on New Variable Structure Guidance Law
Wang Guangyu. Study on New Variable Structure Guidance Law[J]. Aerospace Control, 2005, 23(3): 14-19
Authors:Wang Guangyu
Affiliation:Wang Guangyu Institute of Command and Technology of Equipment,Beijing 101416
Abstract:A new variable structure guidance law (VSG), based on nonlinear relative kinematics, is proposed. The proposed guidance law only uses the information of the target acceleration bound, therefore the precise measuring of target acceleration during interception is not required, namely, the robustness to target maneuver is achieved. Like proportional navigation guidance (PNG), the new guidance law, which utilizes line-of-sight (LOS) measurement only, is simple to implement. Numerical simulations show that the variable structure guidance law has much better performance compared to proportional navigation.
Keywords:Nonlinear relative kinematics equations Robustness Variable structure control Guidance law
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