利用地球紫外和恒星可见光的卫星自主导航

孙俊; 张世杰; 李葆华

doi:10.3788/OPE.20132105.1192

您当前的位置：

首页 >

文章列表页 >

利用地球紫外和恒星可见光的卫星自主导航

微纳技术与精密机械 | 更新时间：2020-08-12

- 利用地球紫外和恒星可见光的卫星自主导航
- Autonomous navigation based on star light and ultraviolet earth sensors
- 光学精密工程 2013年21卷第5期页码：1192-1198
- 作者机构：
  
  哈尔滨工业大学航天学院,黑龙江哈尔滨,150001
- 作者简介：
- 基金信息：
  
  863基金()
- DOI：10.3788/OPE.20132105.1192
  中图分类号： V241.626;V448.22
- 收稿日期：2012-11-29，
  
  修回日期：2013-01-15，
  
  网络出版日期：2013-05-24，
  
  纸质出版日期：2013-05-15
- 稿件说明：
移动端阅览
孙俊张世杰李葆华. 利用地球紫外和恒星可见光的卫星自主导航[J]. 光学精密工程, 2013,21(5): 1192-1198

SUN Jun ZHANG Shi-jie LI bao-hua. Autonomous navigation based on star light and ultraviolet earth sensors[J]. Editorial Office of Optics and Precision Engineering, 2013,21(5): 1192-1198
孙俊张世杰李葆华. 利用地球紫外和恒星可见光的卫星自主导航[J]. 光学精密工程, 2013,21(5): 1192-1198 DOI： 10.3788/OPE.20132105.1192.

SUN Jun ZHANG Shi-jie LI bao-hua. Autonomous navigation based on star light and ultraviolet earth sensors[J]. Editorial Office of Optics and Precision Engineering, 2013,21(5): 1192-1198 DOI： 10.3788/OPE.20132105.1192.

摘要

提出一种利用地球紫外波段和恒星可见光波段为卫星进行自主导航的方法，该导航方法利用视场1观测恒星可见光波段，视场2观测地球紫外波段。在视场1利用星敏感器全天球识别算法识别所有恒星星像，识别结果的光轴指向作为恒星矢量；视场2被用来对地球紫外波段轮廓成像，计算得到地心矢量在卫星本体坐标系中的方向。最后，利用卫星轨道动力学方程和扩展卡尔曼滤波器来计算卫星轨道参数。对一紫外敏感器进行的实验表明，与利用红外地平仪和恒星可见光的自主导航方法相比，该方法的位置误差由1 000 m减小到500 m，速度误差由100 m/s减小到40 m/s，而且消除了由于太阳光与地平线夹角带来的周期误差，因此，该方法具有很好的鲁棒性。

Abstract

An autonomous navigation algorithm is proposed using the sensor with functions of a star sensor and an ultraviolet earth sensor. The sensor has two Field of Views (FOVs ) named FOV1 and FOV2. The FOV1 is used for star sensor and for calculating the optical axis direction of the FOV1. The FOV2 is used for ultraviolet earth sensor and for calculating the vector of the earth. The state equation of integrated system is established by the deduced orbit dynamic model based on orbit six elements and the attitude kinematic model. Then

the observed equation of integrated system is established by using the difference of the measurement value and the estimated value

and the satellite orbit parameters were calculated according to the Discrete Extend Kalman Filter(DEKF)algorithm. An experiment on the ultraviolet sensor shows that not only the errors of satellite positions is improved from 1 000 m to 500 m and the errors for satellite velocities are improved from 100 m/s to 40 m/s

but also the errors of periodic sine resulted from the angle between the sun light and ground level is eliminated. These results show the algorithm to be well robust.

关键词

Keywords

references

WHITE R L, GOUNLEY R B. Satellite Autonomous Navigation with SHAD [M]. The Charles Stark Draper Laboratory, 1987.[2]LEON H S, MICHAEL J R, STUART C S, et al.. Lossless information fusion for active ranging and detection systems [J]. IEEE Transactions on Signal Processing，2006，54(10):3980-3990.[3]MARK L， PSIAKI. Test of magnetometer/sun-sensor orbit determinatin using flight data [J]. Journal of Guidance, Control and Dynamics. 2002, 25(3):582-590.[4]JULIE K. DEUTSCHMANN. Evaluation of attitude and orbit estimation using actual earth magnetic field data [J]. Journal of Guidance, Control, and Dynamics, 2001, 24(3):616-623.[5]周凤岐, 赵黎平, 周军. 基于星光大气折射的卫星自主轨道确定[J]. 宇航学报, 2002, 23(4):20-23.ZHOU F Q, ZHAO L P, ZHOU J. Autonomous orbit determination for earth satellites by starlight atmospheric refraction[J]. Journal of Astronautics, 2002, 23(4):20-23. (in Chinese)[6]王鹏, 张迎春. 基于星敏感器/红外地平仪的自主导航算法研究[J]. 系统工程与电子技术, 2008, 30(8):1514-1518.WANG P, ZHANG Y CH. Research on autonomous navigation algorithm based on star sensor and infrared horizon sensor[J]. Systems Engineering and Electronic, 2008, 30(8):1514-1518. (in Chinese)[7]LIE C C E. Star trackers for attitude determination[J]. IEEE AES Systems Magzine, 1995,31(6): 10-16.[8]XIE J F, JIANG W SH. The analysis of the error sources affecting the accuracy of attitude determined by star sensor \[C\]. Geoinformatics 2007: Remotely Sensed Data and Information, SPIE. 2007, 675249-1.[9]钟兴, 贾继强, 金光,等. 机载导航白天星敏感器的探测性能及总体设计[J]. 光学精密工程, 2011, 19(12):2900-2906.ZHONG X, JIA J Q, JIN G, et al.. Detecting performance and overall design of airborne daylight star sensor for navigation [J]. Opt. Precision Eng., 2011, 19(12):2900-2906. (in Chinese)[10]刘英, 王靖, 曲锋, 等. 广角f-静态红外地平仪镜头的光学设计[J]. 光学精密工程, 2010, 18(6):1243-1248.LIU Y, WANG J, QU F, et al.. Optical design of high precision wide-angle lens for static infrared earth sensor [J]. Opt. Precision Eng., 2010, 18(6):1243-1248. (in Chinese)[11]WANG CH H，LIU R，LI B H, et al.. A geomagnetic positioning method with adaptive genetic algorithm \[C\]. 2010 3nd International Symposium on Systems and Control in Aerospace and Astronautics, ISSCAA, 2010:1014-1018.

浏览量

200

下载量

CSCD

文章被引用时，请邮件提醒。

提交

工具集

关联资源

星敏感器CMOS电路板靶面自动装调系统

基于相似三角形的星图识别

基于多特征匹配的快速星图识别算法

基于多特征匹配的快速星图识别

应用非线性优化算法自主标定星敏感器