确定地球同步自旋卫星姿态的一种方法
An Attitude Determination Method of Spin-Stabilized Geostationary Satellite
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摘要: 本文提出一种同时利用地球角θe、太阳角θs和星日-星地转动角λse三种姿态测量信息, 确定卫星姿态的方法.该法算式简易,可唯一地确定卫星姿态.消除了采用两种姿态测量信 息的姿态确定方法所引起的高相关和低测量密度的不良区域.本文方法仅有太阳矢量和地球 矢量共线的几何限制,能方便地把λse引入滤波器.通过数字仿真,表明此法可得到良好的姿 态确定精度及滤波估计.Abstract: In this paper a method is presented, in which the rotation angle from sun-earth midscan λse in addition to the earth angle θe and sun angle θs are simultaneously used for determinating spinstabilized geostationary satellite attitude. This method gives uniquely one unambiguous attitude. Solution, simplifies the algorithm, eliminates regions of high correlation and low measurement density occuring when using two attitude measurements, and provides geometric condition where singularity occures only if the earth and sun vectors are co-linear. By this method, the mothod, the angle λse is conveniently incorporated into the kalman or least square filter. Digital simulation showed that better accuracy of attitude determination and filter estimation can be obtained by this method.
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