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飞行器落角与撞击时间控制研究
引用本文:施建洪,张友安,梁勇.飞行器落角与撞击时间控制研究[J].海军航空工程学院学报,2011,26(4):398-404.
作者姓名:施建洪  张友安  梁勇
作者单位:海军航空工程学院控制工程系,山东烟台,264001
基金项目:中国博士后科学基金会资助项目
摘    要:对色行器落角与撞击时间控制相关问题进行了综述,包括带落角约束的导引问题、带时间约束的导引问题、带落角与时间约束的导引问题、剩余时间估计问题和欠驱动系统的轨迹跟踪控制问题。针对速度不确定飞行器落角与时间控制问题,从航路规划的角度提出了几个值得进一步研究的问题。

关 键 词:导引  落角控制  撞击时间控制  轨迹跟踪  剩余时间估计  欠驱动系统

Research on Impact Angle Control and Impact Time Control for Aircraft
SHI Jian-hong,ZHANG You-an and LIANG Yong.Research on Impact Angle Control and Impact Time Control for Aircraft[J].Journal of Naval Aeronautical Engineering Institute,2011,26(4):398-404.
Authors:SHI Jian-hong  ZHANG You-an and LIANG Yong
Institution:SHI Jian-hong,ZHANG You-an,LIANG Yong(Department of Control Engineering,NAAU,Yantai Shandong 264001,China)
Abstract:Impact angle control and impact time control related problems for aircraft were surveyed, including the guidance problem with impact angle constraint, guidance problem with impact time constraint, guidance problem with impact angle and time constraint, estimated time remaining problem, and trajectory tracking control problem for under-actuated system. Aiming at impact angle control and impact time aircraft with uncertain velocity, several valued problems for further research were pointed out from route planning control for the view of
Keywords:guidance  impact angle control  impact time control  trajectory tracking  estimated timeremaining  under-actuated system
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