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飞网抛射过程母卫星姿态干扰分析与姿态控制 被引量：4

STUDY ON ATTITUDE DISTURBANCE AND CONTROL OF MOTHER SATELLITE DURING SPACE NET PROJECTING
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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. Space net capturing is a novel technique for spacecraft capturing. In this paper, the disturbance imposed on the mother satellite, and the induced attitude control problem of the satellite, are investigated. Attention is focused on the dynamic process of mass ejection. The main factors affecting the performance of the net are analyzed and the model of the disturbance torque is developed. A sliding mode controller is developed to stabilize the attitude of the satellite and rigid mathematical proof is provided. Numerical simulation is conducted which demonstrates the effectiveness of the proposed algorithm.
作者 高智杰 孙富春 闵海波 王士星
机构地区 清华大学计算机科学与技术系 第二炮兵装备研究院
出处 《力学学报》 EI CSCD 北大核心 2013年第3期434-441,共8页 Chinese Journal of Theoretical and Applied Mechanics
基金 国家自然科学基金资助项目(60904083 61203354)~~
关键词 飞网 母卫星 抛射 姿态控制 滑模控制 space net, mother satellite, projecting, attitude control, sliding mode
分类号 V423 [航空宇航科学与技术—飞行器设计]
  • 相关文献

参考文献12

  • 1Nakasuka 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.
  • 2Nakasuka 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.
  • 3Nakasuka 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.
  • 4于绍华.航天飞行器相对运动动力学及其控制方法[J].宇航学报,1995,16(3):1-7. 被引量：4
  • 5Mankala KK, Agrawal SK. Dynamic modeling and simulation of impact in tether net gripper systems. Mulitbody System Dynamics, 2003, 11(3): 235-250.
  • 6Sorensen J, Kirk E 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.
  • 7Westerhoff 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.
  • 8Bishchof B, Starke J, Guenther H, et al. ROGER-robotic geosta- tionary orbit restorer. In: Proceedings of the 8th ESA Workshop on Advanced Space Technologies for Robotics and Automation. TheNetherlands, November 2-4, 2004, 1214-1218.
  • 9Bonometti J, Sorensen K, Dankanich J. 2006 Status of the mo- mentum exchange electrodynamic re-boost (MXER) tether devel- opment. In: Proceedings of 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Sacramento, Alifornia, July 9- 12, 2006, 451-468.
  • 10Kassebom 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 Astronau- tical Federation, the International Academy of Astronautics, and the International Institute of Space Law, Bremen, Germany, Sep. 29-30, 2003. 279-285.

二级参考文献24

  • 1于绍华.全方位自主交会的控制方法[J].宇航学报,1993,14(3):10-17. 被引量：7
  • 2Jones T C,Bart-Smith H,Mikulas M,Watson J.Finite element modeling and analysis of large pretensioned space structures[J].Journal of Spacecraft and Rockets,2007,44(1):183-193.
  • 3Nakasuka S,Aoki T,Ikeda I,Tsuda Y,Kawakatsu,Y.Furoshiki satellite-a large membrane structure as a novel space system[J].Acta Astronautica,2001,48(5-12):461-468.
  • 4Nakasuka S,Funase R,Nakada K,Kaya N,Mankins J C.Large membrane furoshiki satellite applied to phased array antenna and its sounding rocket experiment[J].Acta Astronautica,2006,58 (8):395-400.
  • 5Nakasuka S,Funane T,Nakamura Y,Nojira Y,Sahara H,Sasaki F,Kaya N.Sounding rocket flight experiment for demonstrating furoshiki satellite for large phased array antenna[J].Acta Astronautica,2006,59(1-5):200-205.
  • 6Mattias Cardsback and Gunnar Tibert.Deployment control of spinning space webs[J].Journal of Guidance,Control,and Dynamics,2009,32(1).
  • 7The Grapple,Retrieve and Secure Payload(GRASP) Experiment,http://www.tethers.com/GRASP.html[Z].
  • 8Robotic GEO Stationary Orbit Restores (ROGER),28 November 2006.http://www.esa.int/TEC/Robotica/SEMTWLKKKSE_O.html[Z].
  • 9Escalona J L,Hussien H,Shabana A A.Application of the absolute nodal coordinate formulation to multibody system dynamics[J].J.Sound Vib.1998,214:833-851.
  • 10Shabana A A,Yakoub R Y.Three dimensional absolute nodal coordinate formulation for beam elements:theory[J].ASME J.Mech.Des.2001,123:606-613.

共引文献91

同被引文献37

  • 1Sinn T,McRobb M , Wujek A. Results of REXUS12s suaineadhexperiment deployment of a spinning space web in micro gravityconditions [ C] //63 rd International Astronautical. Congress. Na-ples ,Italy : The Suaineadh Team, 2012.
  • 2Mankala K K, Agrawal S K. Dynamic modeling and simulation ofimpact in tether net/gripper systems [ J ] . Multibody System Dy-namics ,2004,11(3) :235 -250.
  • 3Summerer L, Purcell 0,Vasile M , et al. Making the first stepstowards solar power from space-microgravity experiments testing thedeployment of large antennas[ C] //60th International Astronauti-cal Congress. Daejeon, Korea : International Astronautical Federa-tion ,2009.
  • 4Gardsback M , Tibert G. Optimal deployment control of spinningspace webs and membranes [ J ]. Journal of Guidance, Control,and Dynamics, 2009, 32(5) :1519 - 1530.
  • 5Gardsback M , Tibert G. Deployment control of spinning spacewebs[ J ] . Journal of Guidance, Control, and Dynamics, 2009 ,32(1) :40 -50.
  • 6Palmerini G B , Sgubini S, Sabatini M. Space webs based on rota-ting tethered formations [ J ]. Acta Astronautica,2009,65(1/2):131 -145.
  • 7Sakamoto H, Natori M C , Kadonishi S, et al. Folding patterns ofplanar gossamer space structures consisting of membranes andbooms [ J ] ? Acta Astronautica,2014 , 94 (1) : 34 - 41.
  • 8Haraguchi D , Sakamoto H , Shirasawa Y , et al. Design criteria forspin deployment of gossamer structures considering nutation dy-namics [ C ] // AIAA Guidance, Navigation, and Control Confer-ence. Toronto, Canada : American Institute of Aeronautics and As-tronautics ,2010.
  • 9Zhai G , Zhang J R, Zhang Y. Circular orbit target capture usingspace tether-net system [ J ] . Mathematical Problems in Engineer-ing, 2013,2013(4) :1 -11.
  • 10翟光,仇越,梁斌,李成.空间飞网捕获机器人系统时变惯量姿态动力学研究[J].宇航学报,2008,29(4):1131-1136. 被引量：17

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二级引证文献25

力学学报
2013年 第3期

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