Modeling and simulation research of missile with deflectable nose

Jian Guo Guo, Yuan Jun He, Jun Zhou

科研成果: 书/报告/会议事项章节会议稿件同行评审

2 引用 (Scopus)

摘要

With respect to a kind of missile with deflectable nose, six-degree-of-freedom dynamics mathematical model including deflectable nose dynamic was established using momentum principle, and guidance system model was presented, at the same time the whole attitude control system with deflectable nose was designed based on variable structure control theory. In order to prove the correctness of the validity of the altitude control strategy, under the environment of MATLAB6.5/SIMULINK, the six-degree-of-freedom digital simulation system was studied and developed for missile with deflectable nose. Finally simulation about non-maneuverable target and the snake-shape maneuverable target were conducted; the results validate the strong maneuverability and intercepting capability of the supersonic missile with deflectable nose, and show the designed control method was effective to the attitude control system.

源语言英语
主期刊名Proceedings - 2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009
86-89
页数4
DOI
出版状态已出版 - 2009
活动2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009 - Shanghai, 中国
期限: 20 11月 200922 11月 2009

出版系列

姓名Proceedings - 2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009
2

会议

会议2009 IEEE International Conference on Intelligent Computing and Intelligent Systems, ICIS 2009
国家/地区中国
Shanghai
时期20/11/0922/11/09

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