Volume 43 Issue 6
Jun.  2017
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WANG Youliang, LI Mingtao, ZHENG Jianhua, et al. Compensation method of in-track coupling effect of cross-track maneuver for formation-flying satellites[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(6): 1165-1172. doi: 10.13700/j.bh.1001-5965.2016.0437(in Chinese)
Citation: WANG Youliang, LI Mingtao, ZHENG Jianhua, et al. Compensation method of in-track coupling effect of cross-track maneuver for formation-flying satellites[J]. Journal of Beijing University of Aeronautics and Astronautics, 2017, 43(6): 1165-1172. doi: 10.13700/j.bh.1001-5965.2016.0437(in Chinese)

Compensation method of in-track coupling effect of cross-track maneuver for formation-flying satellites

doi: 10.13700/j.bh.1001-5965.2016.0437
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  • Corresponding author: LI Mingtao, E-mail:limingtao@nssc.ac.cn
  • Received Date: 23 May 2016
  • Accepted Date: 15 Jul 2016
  • Publish Date: 20 Jun 2017
  • Tetrahedron formation has an important application in the space physical three-dimensional collaborative detection. Formation keeping control must be carried out to guarantee the detecting efficiency. However, the in-track coupling effect of cross-track maneuver can cause the drift along the in-track direction, thus making the deterioration of geometric characteristic, and having a bad effect on the detecting efficiency. An analytical compensation method for formation-flying satellites was designed to eliminate the in-track drift caused by coupling effect of cross-track maneuver, and achieve the accurate formation initialization reconfiguration and formation keeping control under J2 perturbation. The numerical simulation results show that the method is simple and efficient to eliminate the in-track drift caused by cross-track maneuver under J2 perturbation, and can achieve more accurate formation control.

     

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