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Determining the characteristics of the initial fixed-focus of laser beam riding guidance information field

Determining the characteristics of the initial fixed-focus of laser beam riding guidance information field
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摘要 Determining characteristics of the initial fixed-focus are a key technique for the design of laser beam riding guidance missile. Through analyzing the effects of the initial cone information field in guidance and control system of missile, those effects are considered as an approximate lead com- pensation network. The position and time of guidance spot initial fixed-focus can be designed. This method is applied to determine the characteristics of the initial fixed-focus of laser information field for a laser beam guidance gun-launched missile. The results of design and simulation show that the initial cone information field apparently speeds up convergence on the initial trajectory, and provides a guarantee for the implementation of minimum range index of a missile system. Determining characteristics of the initial fixed-focus are a key technique for the design of laser beam riding guidance missile. Through analyzing the effects of the initial cone information field in guidance and control system of missile, those effects are considered as an approximate lead com- pensation network. The position and time of guidance spot initial fixed-focus can be designed. This method is applied to determine the characteristics of the initial fixed-focus of laser information field for a laser beam guidance gun-launched missile. The results of design and simulation show that the initial cone information field apparently speeds up convergence on the initial trajectory, and provides a guarantee for the implementation of minimum range index of a missile system.
出处 《Journal of Beijing Institute of Technology》 EI CAS 2013年第1期6-11,共6页 北京理工大学学报(英文版)
基金 Supported by the Ministerial Level Foundation(62201070412)
关键词 laser beam riding guidance laser information field lead-in trajectory missile guidanceand control system gun-launched missile laser beam riding guidance laser information field lead-in trajectory missile guidanceand control system gun-launched missile
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