Research on autonomous navigation method based on magnetometer and sun sensor

被引：2
|
作者：
Wang, Peng [1 ]
Zhang, Ying-Chun [2 ]
机构：
[1] School of Instrument Science and Engineering, Southeast University
[2] School of Astronautics, Harbin Institute of Technology
来源：
Xi Tong Gong Cheng Yu Dian Zi Ji Shu/Systems Engineering and Electronics | 2013年 / 35卷 / 01期
关键词：
Autonomous navigation; Information fusion; Magnetometer; Sun sensor;
D O I：
10.3969/j.issn.1001-506X.2013.01.22
中图分类号：
学科分类号：
摘要：
The magnetic field vector is a function of the satellite's position. Autonomous low earth orbit satellite navigation can be achieved based on the measurement data of the onboard three axis magnetometer and international geomagnetic reference field. Because the earth's magnetic field is indefinable and long term variability, the navigation precision is limited by only using single magnetometer. A new information fusion method-based autonomous navigation method and filter algorithm is presented by using measuring information of the magnetometer and sun sensor in sun shining area form and sun shadow area form. The integrated navigation method and algorithm are designed and simulated. The computer simulation results show that the proposed system can improve the navigation precision and robustness.
引用
收藏
页码：132 / 137
页数：5
相关论文
共 14 条
  • [1] Lemay J.L., High altitude navigation study, TR0073(3491)-1, (1973)
  • [2] Zhou J., Ge Z.L., Shi G.G., Et al., Key technique and development for geomagnetic navigation, Journal of Astronautics, 29, 5, pp. 1467-1472, (2008)
  • [3] Fang J.C., Ning X.L., Spacecraft Autonomy Principles and Methods of Celestial Navigation, pp. 1-14, (2006)
  • [4] Fang J.C., Ning X.L., Autonomy Celestial Navigation Methods of Deep-Space Exploration Aircraft, pp. 1-15, (2006)
  • [5] Gusarov A., Levron D., Paperno E., Et al., Three-dimensional magnetic field measurements in a single SERF atomic magnetometer cell, IEEE Trans. on Magnetics, 45, 10, pp. 4778-4781, (2009)
  • [6] Deutschmann J., Bar-Itzhck I.Y., Evaluation of attitude and orbit estimation using actual earth magnetic field data, Journal of Guidance, Control and Dynamics, 24, 3, pp. 616-626, (2001)
  • [7] Hee J., Psiaki M.L., Tests of magnetometer/sun-sensor orbit determination using flight data, Proc. of the AIAA Guidance, Navigation, and Control Conference and Exhibit, pp. 1-14, (2001)
  • [8] Psiaki M.L., Autonomous low-earth orbit determination from magnetometer and sun sensor data, Journal of Guidance, Control, and Dynamics, 22, 2, pp. 296-304, (1999)
  • [9] Deutschmann J., Bar-Itzhck I.Y., An innovative method for low cost, autonomous navigation for low earth orbit satellite, Proc. of the AIAA/AAS Astrodynamics Specialist Conference, pp. 1-8, (1998)
  • [10] Gebre-Egziabher D., Elkaim G., Powell J., Et al., Calibration of strapdown magnetometers in magnetic field domain, Journal of Aerospace Engineering, 19, 2, pp. 1-16, (2006)
12