基于脉冲星的日地系平动点轨道自主导航研究  

Autonomous Navigation Based on Pulsar in Libration Point Orbit of Sun-Earth System

作　　者：杨成伟[1,2] 郑建华[1] 李明涛[1] 邓新坪[1,2] 

机构地区：[1]中国科学院空间科学与应用研究中心,北京100190 [2]中国科学院大学,北京100049

出　　处：《空间科学学报》2013年第1期79-84,共6页Chinese Journal of Space Science

基　　金：空间科学预先研究项目资助(XDA04074300)

摘　　要：给出一种利用X射线脉冲星的平动点轨道自主导航算法.分析了X射线脉冲星导航原理,以脉冲到达时间差值为基本观测量,建立导航系统观测方程.在高精度星历模型下,对日地系L_1点Halo轨道建立数学模型,利用基于UD分解的无迹卡尔曼滤波方法进行导航定位,并研究了摄动因素对导航结果的影响.仿真结果表明,在日地系平动点轨道的自主导航中,X射线脉冲星导航是可行的.The application of X-ray pulsar navigation in libration point orbit was discussed. The principle of X-ray pulsar autonomous navigation was analyzed. Difference between the real time and the estimated time of pulse arrival was regarded as the basal measurement. The system model was the full ephemeris dynamic model of Halo orbit around L1 point of the Sun-Earth system. The Unscented Kalman Filter （UKF） based on UD factorization was applied to estimate the state of the system. Perturbation factors were cliscussed to analyze their influence on navigation precision. The simulation results demonstrate that this algorithm is feasible for the autonomous libration point orbit determination in the Sun-Earth system. The method that applies full ephemeris dynamic model and X-ray pulsar-based navigation principle can accomplish the autonomous navigation mission in the libration orbits. Besides, the navigation results are able to converge and the accuracy is enough to meet the navigation demand.

关 键 词：X射线脉冲星 平动点 HALO轨道 自主导航 UD分解无迹卡尔曼滤波 

分 类 号：V448.224[航空宇航科学与技术—飞行器设计]