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Volume 31 Issue 06
Jun.  2005
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Journal of Beijing University of Aeronautics and Astronautics  > 2005  >  31(06): 614-617.
YANG B，JIN F T，LIU Y B，et al. Intelligent solution method based on high-speed aircraft fire control model[J]. Journal of Beijing University of Aeronautics and Astronautics，2024，50（5）：1693-1701 （in Chinese） doi: 10.13700/j.bh.1001-5965.2022.0503
Citation: Li Chenguang, Han Chao. Study on measurement of relative motion of satellite formation flight[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(06): 614-617. (in Chinese)
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Study on measurement of relative motion of satellite formation flight

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

  • Received Date: 26 Feb 2004
  • Publish Date: 30 Jun 2005
    Abstract
  • In satellite formation flight, the measurement and determination of independent relative orbit is one of the most important techniques of formation flight. The traditional techniques of using star sensor, radar and GPS(global positioning system) signal to determine relative orbit are considered. Relative orbit determination which is based on pseudo satellite technique is considered. Pseudo satellite technique means that carrier generators and receivers are assembled onboard, and are used to measure the distance between satellites. In these projects, differential carrier-phase GPS sensors are used, and nonlinear equations are solved by optimization methods. These methods of measurement adapt different situation. On the base of measurement results from previous three projects, using the concept of relative orbit elements, precision of orbit determination is improved by Kalman filter. Emulation calculations indicate that the request of keeping formation can be satisfied, and a part of results is presented.

     

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    • References(1)
  • [1] 张守信.GPS卫星测量定位理论与应用[M].长沙:国防科技大学出版社,1996 Zhang Shouxin. Theory and application of GPS orientation and measurement [M]. Changsha:University of National Defence Technology Press, 1996(in Chinese) [2] Corazzini T, Robertson A, Adams J C, et al. How, GPS sensing for space formation flying . Institute of Navigation GPS-97 . Kansas City, Missouri, 1997 [3] How J P, Twiggs R, Weidow D, et al. ORION:a low-cost demonstration of formation flying in space using GPS . AIAA-98-4398, 1998 [4] Corazzini T, How J P. Onboard GPS signal augmentation for spacecraft formation flying . Proceedings of the Institute of Navigation GPS-98 Conference . Nashville TN, 1998 [5] 韩 潮,肖业伦,杨 宇.编队飞行卫星群的轨道设计及演示验证 ,2002 Han Chao, Xiao Yelun, Yang Yu. Orbit design and demostration validation of satellite formation flight ,2002(in Chinese)
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