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高超声速战术导弹精确制导律设计
引用本文:孟中杰,陈凯,黄攀峰,闫杰. 高超声速战术导弹精确制导律设计[J]. 飞行力学, 2009, 27(2)
作者姓名:孟中杰  陈凯  黄攀峰  闫杰
作者单位:西北工业大学航天学院,陕西,西安,710072
基金项目:国家高技术研究发展计划(863计划),航天支撑基金 
摘    要:高超声速战术导弹以其固有的特点在高速目标拦截上应用前景巨大.如何针对高超声速战术导弹高速度、高不确定性的特点设计精确的制导律是导弹能否摧毁目标的关键.针对高超声速战术导弹和高速机动目标建立了相对运动模型,利用自适应滑模控制理论,设计了导弹的自适应精确制导律,并进行了仿真分析.结果表明,该制导律具有较好的控制效果.

关 键 词:高超声速飞行器  高速机动目标  精确制导  自适应滑模制导律

Design of Accurate Guidance for Hypersonic Vehicle
MENG Zhong-jie,CHEN Kai,HUANG Pan-feng,YAN Jie. Design of Accurate Guidance for Hypersonic Vehicle[J]. Flight Dynamics, 2009, 27(2)
Authors:MENG Zhong-jie  CHEN Kai  HUANG Pan-feng  YAN Jie
Affiliation:College of Astronautics;Northwestern Polytechnical University;Xi'an 710072;China
Abstract:Hypersonic vehicle has a huge foreground in heading off the high speed and highly maneuvering target.How to design an accurate guidance for the vehicle is a key technique for destroy the target under high velocity and uncertainties.As the capability of the target is improved,the missile must have an accurate guidance law to finish the task.The sliding mode control theory had applied abroad in designing an automatic pilot since its excellences such as stability and flexibility.This thesis establishes the mod...
Keywords:hypersonic vehicle  high speed and highly maneuvering target  accurate guidance  adaptive sliding mode guidance law  
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