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柔性太阳帆航天器动力学建模与姿态控制 被引量：10

Study on dynamics modeling and attitude control of flexible solar sail spacecraft
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摘要 对基于控制叶片的太阳帆航天器,推导考虑弹性振动的太阳帆姿态动力学方程和振动方程,利用非约束模态的概念给出了太阳帆航天器动力学方程的求解方法.结合超地球同步转移轨道太阳帆航天器偏航轴对地定向问题,设计了太阳帆俯仰轴的考虑Bang-Bang控制策略的PD控制器,数值仿真结果表明,所设计的基于控制叶片的控制器可以较快、较精确地实现偏航轴对地定向任务. For solar sail spacecraft with control vanes,solar sail attitude dynamics equations considering elastic vibration and vibration equations were deduced.The solutions of solar sail spacecraft dynamics equations were achieved by utilizing the concepts of unconstraint modes.The PD controller with Bang-Bang control strategies was designed considering the problems of yaw axis earth-pointing of solar sail on super-synchronous transfer orbit.Numerical simulation shows that the designed controller based on control vanes is capable of controlling the yaw axis earth-pointing fast and accurately.
作者 崔乃刚 刘家夫 荣思远
机构地区 哈尔滨工业大学航天工程系
出处 《哈尔滨工业大学学报》 EI CAS CSCD 北大核心 2011年第7期1-5,共5页 Journal of Harbin Institute of Technology
基金 国家自然科学基金资助项目(10772057)
关键词 太阳帆航天器 姿态动力学方程 振动方程 控制叶片 姿态控制 solar sail spacecraft attitude dynamics equations vibration equations control vanes attitude co-ntrol
分类号 V412.4 [航空宇航科学与技术—航空宇航推进理论与工程]
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参考文献13

  • 1MCLNNES C. Solar sailing: technology, dynamics, and mission applications [M]. New York : Springer-Praxis, 1999.
  • 2骆军红,李晓东,冯军华.太阳帆航天器被动姿态控制研究[J].飞行力学,2008,26(5):47-50. 被引量：3
  • 3METI'LER E, ACIKMESE A B, PLOEN S R. Attitude dynamics and control of solar sails with articulated vanes [ C ]//AIAA Guidance, Navigation, and Control Confer- ence and Exhibit. San Francisco : [ s. n. ] , 2005.
  • 4WIE B. Solar sail attitude control and dynamics : Part 2 [J]. Journal of Guidance, Control, and Dynamics, 2004, 27(4):536-544.
  • 5WIE B. Dynamic modeling and attitude control of solar sail spacecraft : Part I [ C ]//AIAA Guidance, Naviga- tion, and Control Conference and Exhibit. Monterey: [ s. n. ] , 2002.
  • 6METTLER E, PLOEN S R. Solar sail dynamics and con- trol using a boom mounted bus articulated by a hi-state two-axis gimbal and reaction wheels [ C]//AIAA/AAS Astrodynamics Specialist Conference and Exhibit. Monterey : [ s. n. ]. 2002.
  • 7WIE B. Dynamic modeling and attitude control of solar sail Spacecraft : Part II[ C ]//AIAA Guidance, Naviga- tion, and Control Conference and Exhibit. Monterey: [ s. n. ], 2002.
  • 8WIE B, MURPHY D, PALUSZEK M, et al. Robust at- titude control systems design for solar sails: Part l [ C ]//AIAA Guidance, Navigation, and Control Confer- ence and Exhibit. Providence, Rhode Island: [ s. n. ] , 2004.
  • 9WIE B, MURPHY D. Solar-sail attitude control design for a sail flight validation mission [ J]. Journal of Space- craft and Rockets, 2007, 4(44), :809-821.
  • 10刘暾 杨大明.挠性卫星动力学及姿态控制模型的建立.哈尔滨工业大学学报,1985,17(8):1-17.

二级参考文献11

  • 1刘暾,杨大明.带挠性附件卫星的模型化及截断[J].宇航学报,1989,10(4):87-95. 被引量：9
  • 2　Enrique Barbieri．Unconstrained and constrained mode expansions for a flexibleslewing link [J]．Transaction of ASME，1998,110.
  • 3　刘　暾，杨大明,张为平．On optimal control strategy of maneuver ofsatellites with flexible appendages [C].Proceedings of PISSTA，June 7-10，1987，Beijing，China．
  • 4Victoria L Coverstone,John E Prussing. Technique for Escape from Geosynchronous Transfer Orbit Using a Solar Sail [ J ]. Journal of Guidance, Control, and Dynamics, 2003,26(4) :628-634.
  • 5Christoph Sickinger, Lars Herbeck, Elmar Breitbach. Structural Engineering on Eeployable CFRP Booms for a Solar Propelled Sailcraft [ J ]. Acta Astronautica, 2006,58 ( 4 ) : 185-196.
  • 6Scaglione, Vulpetti. The Aurora Project : Removal of Plastic Substrate to Obtain an All-Metal Solar Sail [ J ]. Acta Astronautica, 1999,44(2-4) : 147-150.
  • 7Robert Gershman, Calina Seybold. Propulsion Trades for Space Science Missions [ J ]. Acta Astronautica, 1999,45 ( 4-9 ) : 541-548.
  • 8Azor. Solar Attitude Control Including Active Nutation Damping in a Fixed-Momentum Wheel Satellite [ A ]. AIAA Guidance, Navigation, and Control Conference [ C ]. Hilton Head Islands,SC, 1992:229-236.
  • 9Bong Wie. Dynamic Modeling and Attitude Control of Solar Sail Spacecraft: Part Ⅰ [ C ]. AIAA Guidance, Navigation and Control Conference and Exhibit, 2002-4572, 2002: 1-2.
  • 10McInnes. Solar Sailing-Orbital Mechanics and Mission Applications [ J ]. Advanced Space Research, 2003,31 ( 8 ) : 1971-1980.

共引文献18

同被引文献109

引证文献10

二级引证文献23

哈尔滨工业大学学报
2011年 第7期

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