Flight range optimization of extended range guided munitions

Qun Li Xia; Zai Kang Qi; De Fu Lin

Flight range optimization of extended range guided munitions

Qun Li Xia^*, Zai Kang Qi, De Fu Lin

^*此作品的通讯作者

宇航学院

Beijing Institute of Technology

科研成果: 期刊稿件 › 文章 › 同行评审

4 引用（Scopus）

摘要

By the study of extended range guided munitions (ERGM) trajccrory characteristics, ERGM free-flight and glide trajectory characteristics are revealed and illustrated. On the basis of free-flight trajectory mathematical model, a two-parameter optimization problem of quadrant elevation and rocket ignition time is studied- Using the atmosphere mathematical model, the best glide-starting point of the downward trajectory is determined, With an optimal control mathematical model, the ERGM optimal glide trajectory is obtained.

源语言	英语
页（从-至）	383-388
页数	6
期刊	Journal of Beijing Institute of Technology (English Edition)
卷	11
期	4
出版状态	已出版 - 12月 2002

其它文件与链接

链接到 Scopus 的出版物

引用此

Xia, Q. L., Qi, Z. K., & Lin, D. F. (2002). Flight range optimization of extended range guided munitions. Journal of Beijing Institute of Technology (English Edition), 11(4), 383-388.

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abstract = "By the study of extended range guided munitions (ERGM) trajccrory characteristics, ERGM free-flight and glide trajectory characteristics are revealed and illustrated. On the basis of free-flight trajectory mathematical model, a two-parameter optimization problem of quadrant elevation and rocket ignition time is studied- Using the atmosphere mathematical model, the best glide-starting point of the downward trajectory is determined, With an optimal control mathematical model, the ERGM optimal glide trajectory is obtained.",

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AU - Lin, De Fu

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N2 - By the study of extended range guided munitions (ERGM) trajccrory characteristics, ERGM free-flight and glide trajectory characteristics are revealed and illustrated. On the basis of free-flight trajectory mathematical model, a two-parameter optimization problem of quadrant elevation and rocket ignition time is studied- Using the atmosphere mathematical model, the best glide-starting point of the downward trajectory is determined, With an optimal control mathematical model, the ERGM optimal glide trajectory is obtained.

AB - By the study of extended range guided munitions (ERGM) trajccrory characteristics, ERGM free-flight and glide trajectory characteristics are revealed and illustrated. On the basis of free-flight trajectory mathematical model, a two-parameter optimization problem of quadrant elevation and rocket ignition time is studied- Using the atmosphere mathematical model, the best glide-starting point of the downward trajectory is determined, With an optimal control mathematical model, the ERGM optimal glide trajectory is obtained.

KW - Free-flight trajectory

KW - Optimal glide trajectory

KW - Parameter optimization

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Flight range optimization of extended range guided munitions

摘要

其它文件与链接

指纹

引用此