A 3D Nonlinear Guidance Law with Impact Terminal Angle Constraints

被引:0
|
作者
Li Xinsan [1 ]
Wang Lixin [1 ]
Chen Ke [1 ]
Yan Xunliang [1 ]
Fan Xiaohu [2 ]
Ding Bangping [2 ]
机构
[1] Second Artillery Engn Univ, Dept 3, Xian, Shaanxi, Peoples R China
[2] Second Artillery Engn Univ, Petty Officer Acad, Qingzhou, Shandong, Peoples R China
来源
2015 CHINESE AUTOMATION CONGRESS (CAC) | 2015年
关键词
guidance; nonlinear optimal control; impact terminal angle constraint; model predictive static programming;
D O I
暂无
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
Generalized model predictive static programming (G-MPSP) technique is presented in this paper in the continuous time framework for rapidly solving a class of 3D nonlinear optimal control problems with hard terminal constraints. A key feature of the technique is backward propagation of a small-dimensional weight matrix dynamics, using which the control history got updated. It leads to a static optimization problem and it is the reason for its high computational efficiency. Various maneuvering ground targets is considered in the simulation studies. The simulation results show that impact angle constraints are met in addition to achieving near zero miss distance and the variation in the lateral acceleration history is quite smooth throughout the engagement.
引用
收藏
页码:2242 / 2246
页数:5
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