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Integrated Guidance and Control for Homing Missiles with Terminal Angular Constraint in Three Dimension Space

  • Northwestern Polytechnical University Xian

科研成果: 书/报告/会议事项章节会议稿件同行评审

1 引用 (Scopus)

摘要

A three dimension integrated guidance and control (3D-IGC) system for homing missiles with terminal angle constraint is designed. Firstly, a nonlinear mathematical model of the homing missile is established. In order to deal with the problem of multiple states regulation of such a nonlinear system, an adaptive multiple sliding surface control methodology is deduced. The frame of 3D-IGC law is accomplished by associating with the backstepping method. The digital simulation results verify that the proposed control law can both satisfy the accuracy of target interception and the constrained conditions of terminal angular. Moreover, it shows strong robustness against parameter uncertainties.

源语言英语
主期刊名Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020
出版商Institute of Electrical and Electronics Engineers Inc.
601-606
页数6
ISBN(电子版)9781728165905
DOI
出版状态已出版 - 3月 2020
活动2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020 - Dalian, 中国
期限: 20 3月 202022 3月 2020

出版系列

姓名Proceedings of 2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020

会议

会议2020 IEEE International Conference on Artificial Intelligence and Information Systems, ICAIIS 2020
国家/地区中国
Dalian
时期20/03/2022/03/20

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