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Volume 33 Issue 10
Oct.  2007
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Journal of Beijing University of Aeronautics and Astronautics  > 2007  >  33(10): 1166-1169.
Xu Ming, Jia Yinghong, Xu Shijieet al. Attitude description and dynamics modeling for Halo-orbit spacecraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(10): 1166-1169. (in Chinese)
Citation: Xu Ming, Jia Yinghong, Xu Shijieet al. Attitude description and dynamics modeling for Halo-orbit spacecraft[J]. Journal of Beijing University of Aeronautics and Astronautics, 2007, 33(10): 1166-1169. (in Chinese)
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Attitude description and dynamics modeling for Halo-orbit spacecraft

  • School of Astronautics, Beijing University of Aeronautics and Astronautics, Beijing 100083, China

  • Received Date: 24 Oct 2006
  • Publish Date: 31 Oct 2007
    Abstract
  • Halo orbit locates about the libration point in the Sun-Earth system and has no orbital plane focusing the Earth, which makes the attitude description and dynamics modeling for Halo-orbit spacecraft is quite different from that for the usual satellite around the Earth. Two different schemes of attitude description were proposed for the spacecraft in the three axis stabilization, sun-orienting scheme (Scheme I, using the Sun and Earth attitude sensors) and rotating-reference scheme (Scheme II, using the Star attitude sensor). So the attitude dynamics can be modeled from the different orbital coordinates defined by the two schemes. The upper limits of relative errors for the two schemes were estimated theoretically: no more than 5% for Scheme I, and 0.005% for Scheme II. A controller was designed for the attitude stabilization to validate the feasibility of the schemes. The research shows that Scheme II is set as the normal mode with the astronomical ephemeris periodically corrected, while Scheme I is used as the alternate device for the failure mode.

     

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  • [1] Farquhar R W, Dunham D W, Guo Y P, et al. Utilization of libration points for human exploration in the sun-earth-moon system and beyond [J]. Acta Astronautica, 2004, 55:687-700 [2] Richardson D L. Analytical construction of periodic orbits about the collinear points [J]. Celestial Mechanics, 1980, 22:241-253 [3] Mihai P, Vladimir C. The domain of initial conditions for the class of three-dimensional halo periodical orbits [J]. Acta Astronautica, 1995, 36:193-196 [4] 徐明, 徐世杰. 地-月系平动点及Halo轨道的应用研究[J]. 宇航学报, 2006, 27(4):696-699 Xu Ming, Xu Shijie. The application of libration points and halo orbits in the earth-moon system to space mission design [J]. Journal of Astronautics, 2006, 27(4):696-699 (in Chinese) [5] 章仁为. 卫星轨道姿态动力学与控制[M]. 北京: 北京航空航天大学出版社, 1998 Zhang Renwei. Orbit and attitude dynamics and control of satellite [M]. Beijing: Press of Beijing University of Aeronautics and Astronautics, 1998 (in Chinese) [6] Carpenter J R, Folta D C, Moreau M C, et al. Libration point navigation concepts supporting the vision for space exploration Astrodynamics Specialist Conference and Exhibit. Reston: AIAA/AAS, 2004: 179-193
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