Integrated guidance and control design for guided bomb with terminal angle constraint

被引：0
作者：
Han, Yang [1 ]
Zheng, Zhiqiang [1 ]
Chong, Yuhai [2 ]
机构：
[1] Natl Univ Def Technol, Coll Mechatron Engn & Automat, Changsha, Hunan, Peoples R China
[2] Xichang Satellite Launch Ctr, Xichang, Sichuan Provinc, Peoples R China
来源：
2015 IEEE INTERNATIONAL CONFERENCE ON INFORMATION AND AUTOMATION | 2015年
关键词：
integrated guidance and control; theta - D suboptimal method; pitch plane; terminal angle constraint;
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：
Integrated guidance and control laws have the potential to improve the overall performance of missile systems by taking advantage of the synergism existing between the subsystems. This paper examines the proposed integrated guidance and control by using theta - D suboptimal method to the engagement of ground-fixed target. First, the basic longitudinal mathematical integrated guidance and control model is established. next, a new suboptimal control method, called theta - D, is employed to obtain an approximate closed form solution to this integrated guidance and control problem based on approximations to the Hamilton-Jacobi-Bellman equation. Finally, the performance of designed algorithm is verified via numerical simulation, which shows the feasibility and realizability of the proposed method.
引用
收藏
页码：1344 / 1348
页数：5
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