摘要
利用扩展卡尔曼(EKF)滤波原理研究基于天基光学平台对低轨卫星的跟踪问题,根据单星只测角观测值建立了相应的状态模型和观测模型,并进行低轨卫星的跟踪仿真,结果表明:该方法可以获得较高的跟踪精度,这使得基于单星只测角星上滤波跟踪成为可能。
This paper uses Extended Kalman Filter (EKF) in research on tracking of low earth orbit satellites with a single space-based optic platform. Two different observation models are established based on bearings-only detection data. Tracking simulation of a LEO satellite is performed and high tracking accuracy is demonstrated during the simulation. This makes possible bearings-only on-beard filter tracking for a single satellite.
出处
《飞行器测控学报》
2007年第6期70-75,共6页
Journal of Spacecraft TT&C Technology
关键词
只测角
角度变化率
二体运动
EKF滤波
Bearings-Only
Angular Change Rate
Two-Body Theory
Extended Kalman Filter