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飞网抛射过程母卫星姿态干扰分析与姿态控制

高智杰 孙富春 闵海波 王士星

高智杰, 孙富春, 闵海波, 王士星. 飞网抛射过程母卫星姿态干扰分析与姿态控制[J]. 力学学报, 2013, 45(3): 434-441. doi: 10.6052/0459-1879-12-249
引用本文: 高智杰, 孙富春, 闵海波, 王士星. 飞网抛射过程母卫星姿态干扰分析与姿态控制[J]. 力学学报, 2013, 45(3): 434-441. doi: 10.6052/0459-1879-12-249
Gao Zhijie, Sun Fuchun, Min Haibo, Wang Shixing. STUDY ON ATTITUDE DISTURBANCE AND CONTROL OF MOTHER SATELLITE DURING SPACE NET PROJECTING[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(3): 434-441. doi: 10.6052/0459-1879-12-249
Citation: Gao Zhijie, Sun Fuchun, Min Haibo, Wang Shixing. STUDY ON ATTITUDE DISTURBANCE AND CONTROL OF MOTHER SATELLITE DURING SPACE NET PROJECTING[J]. Chinese Journal of Theoretical and Applied Mechanics, 2013, 45(3): 434-441. doi: 10.6052/0459-1879-12-249

飞网抛射过程母卫星姿态干扰分析与姿态控制

doi: 10.6052/0459-1879-12-249
基金项目: 国家自然科学基金资助项目(60904083,61203354).
详细信息
    通讯作者:

    高智杰,博士研究生,主要研究方向:智能控制理论与应用、卫星动力学分析与协同控制.E-mail:zjiegao@163.com

  • 中图分类号: V423

STUDY ON ATTITUDE DISTURBANCE AND CONTROL OF MOTHER SATELLITE DURING SPACE NET PROJECTING

Funds: The project was supported by the National Natural Science Foundation of China (60904083, 61203354).
  • 摘要: 空间飞网是一种新型的空间碎片或漂浮物回收装置. 飞网抛射过程会对母体卫星产生较大的干扰,影响卫星的姿态稳定,因此需要设计具有抗干扰能力的控制律来保证卫星姿态的稳定. 针对空间飞网直接抛射展开过程,分析了影响飞网抛射效果的主要因素,并建立了飞网发射所产生的干扰力矩模型. 针对卫星的控制要求,建立了卫星姿态控制系统的模型,设计了滑模变结构控制器,并给出数学推导过程. 最后,通过仿真对姿态干扰及控制器控制性能进行了分析研究,结果表明,设计的控制器能够保证卫星的稳定,满足设计指标要求.

     

  • Nakasuka S, Aoki T, Ikeda I, et al. "Furoshiki Satellite"——A large membrane structure as a novel space system. Acta Astronautica, 2001, 48(5-12): 461-468
    Nakasuka S, Funase R, Nakada K, et al. Large membrane "Furoshiki Satellite" applied to phased array antenna and its sounding rocket experiment. Acta Astronautica, 2006, 58(8): 395-400  
    Nakasuka S, Funane T, Nakamura Y, et al. Sounding rocket flight experiment for demonstrating "Furoshiki Satellite" for large phased array antenna. Acta Astronautica, 2006, 59(1-5): 200-205  
    于绍华.航天飞行器相对运动动力学及其控制方法.宇航学报, 1995, 16(3): 1-7 (Yu Shaohua. The dynamics and control of spacecraft of relative motion. Journal of Astronautics, 1995, 16(3): 1-7 (in Chinese))
    Mankala KK, Agrawal SK. Dynamic modeling and simulation of impact in tether net gripper systems. Mulitbody System Dynamics, 2003, 11(3): 235-250
    Sorensen J, Kirk F. Conceptual design and analysis of an MXER tether boost station. In: Proceedings of Joint Propulsion Conference and Exhibit, 37th, Salt Lake City, UT, July 8-11, 2001, 391-402
    Westerhoff J. Optimal configuration of MXER tether systems. In: Proceedings of 39th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Huntsville, Alabama, July 20-23, 2003, 522-531
    Bishchof B, Starke J, Guenther H, et al. ROGER-robotic geostationary orbit restorer. In: Proceedings of the 8th ESA Workshop on Advanced Space Technologies for Robotics and Automation. The Netherlands, November 2-4, 2004, 1214-1218
    Bonometti J, Sorensen K, Dankanich J. 2006 Status of the momentum exchange electrodynamic re-boost (MXER) tether development. In: Proceedings of 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, Alifornia, July 9-12, 2006, 451-468
    Kassebom M, Koebel D, Tobehn C, et al. ROGER——An advanced solution for a geostationary service satellite. In: Proceedings of 54th International Astronautical Congress of the International Astronautical Federation, the International Academy of Astronautics, and the International Institute of Space Law, Bremen, Germany, Sep. 29-30, 2003. 279-285
    李俊峰, 蒋方华. 连续小推力航天器的深空探测轨道优化方法综述.力学与实践, 2011, 33(3): 1-6 (Li Junfeng, Jiang Fanghua. Summary of continuous low-thrust deep space exploration spacecraft orbit optimization method. Journal of Mechanics in Engineering, 2011, 33(3): 1-6 (in Chinese))
    于洋, 宝音贺西, 李俊峰. 空间飞网抛射展开动力学建模与仿真.宇航学报, 2010, 31(5): 1289-1296 (Yu Yang, Baoyin Hexi, Li Junfeng. Modeling and simulation of projecting deployment dynamics of space webs. Journal of Astronautics, 2010, 31(5): 1289-1296 (in Chinese))
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出版历程
  • 收稿日期:  2012-09-13
  • 修回日期:  2012-10-23
  • 刊出日期:  2013-05-18

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