Volume 35 Issue 8
Aug.  2009
Turn off MathJax
Article Contents
Li Baojun, Shi Peng, Zhang Hao, et al. Satellites formation reconfiguration with multiple impulses[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(8): 950-952. (in Chinese)
Citation: Li Baojun, Shi Peng, Zhang Hao, et al. Satellites formation reconfiguration with multiple impulses[J]. Journal of Beijing University of Aeronautics and Astronautics, 2009, 35(8): 950-952. (in Chinese)

Satellites formation reconfiguration with multiple impulses

  • Received Date: 27 Jun 2008
  • Publish Date: 31 Aug 2009
  • Satellite formation flying (SFF) reconfiguration using multiple impulses was studied, which was mainly focusing on fuel efficiency.The elliptic reference orbit was considered. First the mathematical description of multiple-burn maneuver was established based on the analytical solution of the Lawden equation. Then object function was constructed as the total fuel which took the form as function of the imposing time and the magnitude of the previous n-2 burns, followed with the problem being solved utilizing the genetic algorithm. Finally the result was transferred into time domain to determine the magnitude, direction and imposing time of each of the impulse vectors. The simulation shows that the algorithm presented could lead to a more efficient method to implement the SFF reconfiguration.

     

  • loading
  • [1] Kapila V, Sparks A G, Buffington J M, et al. Spacecraft formation flying: dynamics and control [J]. Journal of Guidance, Control and Dynamics, 2000, 23(3): 561-564 [2] 林来兴.分布式空间系统和航天器编队飞行辨析[J].航天器工程,2008, 17(4):24-29 Lin Laixing. Study on distributed space systems and spacecraft formation flying [J]. Spacecraft Engineering, 2008, 17(4):24-29(in Chinese) [3] Ichimura Y, Ichikawa A. Optimal impulsive relative orbit transfer along a circular orbit [J]. Journal of Guidance, Control and Dynamics, 2008,31(4):1014-1027 [4] 孟云鹤,韩宏伟,戴金海. 近地轨道航天器编队构形重构的一种四冲量控制方法[J].宇航学报, 2008, 29(2):505-510 Meng Yunhe, Han Hongwei, Dai Jinhai. A four-impulses control method for reconfiguration of LEO spacecraft formation flying[J]. Journal of Astronautics, 2008, 29(2):505-510(in Chinese) [5] Vaddi S S, Alfriend K T,Vadali S R. et al. Formation establishment and reconfiguration using impulsive control [J]. Journal of Guidance, Control and Dynamics,2005, 28(2):262-268 [6] Lawden D F. Optimal trajectories for space navigation[M]. London: Butterworths, 1963 [7] Carter T E. New form for the optimal rendezvous equations near a keplerian orbit[J]. Journal of Guidance, Control, and Dynamics, 1990, 13(1): 183-186 [8] 崔海英,李俊峰,高云峰.基于Lawden方程的理想编队队形设计[J].清华大学学报(自然科学版),2006,46(2):271-275 Cui Haiying, Li Junfeng, Gao Yunfeng. Ideal relative trajectories design based on Lawden-s equations[J]. Journal Of Tsinghua University(Science & Technology), 2006, 46(2):271-275(in Chinese) [9] Yamanak K, Ankersen F.New state transition matrix for relative motion on an arbitrary elliptical orbit[J]. Journal Of Guidance, Control, and Dynamics, 2002, 25(1):60-66
  • 加载中

Catalog

    通讯作者: 陈斌, bchen63@163.com
    • 1. 

      沈阳化工大学材料科学与工程学院 沈阳 110142

    1. 本站搜索
    2. 百度学术搜索
    3. 万方数据库搜索
    4. CNKI搜索

    Article Metrics

    Article views(2647) PDF downloads(895) Cited by()
    Proportional views
    Related

    /

    DownLoad:  Full-Size Img  PowerPoint
    Return
    Return