Journal of Systems Engineering and Electronics ›› 2012, Vol. 34 ›› Issue (5): 1001-1006.doi: 10.3969/j.issn.1001-506X.2012.05.26

• 制导、导航与控制 • 上一篇    下一篇

基于信息融合的自主天文导航方法

王鹏1, 张迎春2   

  1. 1. 东南大学仪器科学与工程学院, 江苏 南京 200096;
    2. 哈尔滨工业大学航天学院, 黑龙江 哈尔滨 150080
  • 出版日期:2012-05-23 发布日期:2010-01-03

Method of autonomous celestial navigation based on information fusion

WANG Peng1, ZHANG Ying-chun2   

  1. 1. School of Instrument Science and Engineering, Southeast University, Nanjing 200096, China; 2. Institute of Astronautics, Harbin Institute of Technology, Harbin 150080, China
  • Online:2012-05-23 Published:2010-01-03

摘要:

直接敏感地平和间接敏感地平是典型的两种自主天文导航方法,直接敏感地平简单可靠,但是由于地球敏感器精度较低,因此导航精度不高|利用星光折射的间接敏感地平精度较高,但是折射星数量有限并且观测时段较短。针对上述两种方法的缺点,提出一种基于信息融合的自主天文导航方法。当观测不到折射星时引入新信息,弥补间接敏感地平自主导航的不足。通过对多种导航模式进行数值仿真与分析,验证所设计方法提高了系统的导航精度和可靠性。

Abstract:

Direct sensing horizon and indirect sensing horizon are two typical kinds of autonomous celestial navigation method.  Direct sensing horizon is simply and reliable, but the navigation precision that depends mainly on earth sensor is lower.  Indirect sensing horizon gets horizon information by observing atmosphere refraction stellar using the star sensor.  Because the numbers of refraction stellar and observing time are limited, the observed information is discontinuous. A  new method of autonomous celestial navigation using both of the two methods based on information fusion is presented. The  new information is imported when refraction stars cannot be observed. Simulation results show that the proposed method  can improve the precision and reliability of the navigation system.