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一种基于光学成像敏感器多目标视线角测量的相对导航方法

A Novel Relative Navigation Method Using Angles Observations from Vision Sensor
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摘要 针对基于光学成像敏感器测量的相对导航问题,提出一种直接采用光学敏感器多目标视线角测量信息,利用UKF滤波方法设计滤波器,对相对位置、相对速度和相对姿态等相对状态进行估计的相对导航方法。将所提出的方法应用于月球交会对接平移靠拢段的相对导航,通过数学仿真验证了所提出方法的有效性,对实际工程应用具有理论参考价值。 A novel UKF filter is designed to estimate the relative position, velocity and attitude of chaser of the target spacecraft, and the angles from vision sensors are used as measurement information. The new filter is applied to the closing phase of lunar rendezvous and docking, and the simulation results show the validity of the method. The new method is a valuable reference for the project application.
作者 刘涛 胡海霞 王颖 王大轶
机构地区 北京控制工程研究所 空间智能控制技术国家级重点试验室
出处 《航天控制》 CSCD 北大核心 2013年第2期42-48,55,共8页 Aerospace Control
关键词 光学成像敏感器 视线角 相对导航 Vision sensor Angles observations Relative navigation
分类号 V249.3 [航空宇航科学与技术—飞行器设计]
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航天控制
2013年 第2期

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