Analytical Study of CLOS Guidance Law against Head-on High-Speed Maneuvering Targets

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概要

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• A command to line-of-sight (CLOS) guidance law is developed against head-on high-speed maneuvering targets. Preliminary studies have shown that the aspect angle of the interceptor at lock-on near 180 deg is a fundamental requirement for achieving small miss distance against a very high-speed incoming target. The solutions of missile trajectory obtained before under this guidance scheme seemed tedious and incomplete. Now, in this study, exact and complete solutions which are more general and comprehensive than those obtained before are derived for head-on high-speed maneuvering targets. Some related important characteristics such as lateral acceleration demand and normalized missile acceleration are investigated and discussed. Additionally, illustrated examples of target maneuvering are introduced to easily describe the trajectory of the target. The results obtained in this study are very significant and practical, and will be useful in actual application.

• 社団法人 日本航空宇宙学会の論文
• 2007-08-04

著者

• Lee Sou-chen

  College Of Humanities And Sciences Lunghwa University Of Science And Technology

• CHAO Chia-Chi

  Department of Weapon System Engineering, Chung Cheng Institute of Technology, National Defense Unive

• SOONG Chen-Yaw

  Department of Electronics, China Institute of Technology

• Chao Chia-chi

  Department Of Weapon System Engineering Chung Cheng Institute Of Technology National Defense Univers

• Soong Chen-yaw

  Department Of Electronics China Institute Of Technology

関連論文

• Analytical Study of CLOS Guidance Law against Head-on High-Speed Maneuvering Targets

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