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卫星有效载荷的地位和作用 被引量:4

Status and Function of Satellite Payload
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作者 崔绍春
出处 《航天返回与遥感》 2003年第1期61-65,共5页 Spacecraft Recovery & Remote Sensing
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同被引文献38

  • 1刘霞,罗文彩,赵勇,陈小前.卫星系统总体方案树合成技术研究[J].军民两用技术与产品,2006(8):36-39. 被引量:1
  • 2朱毅麟.微型航天器的公用平台和关键技术[J].中国空间科学技术,1997,17(2):25-32. 被引量:5
  • 3MARKLEY F L,BAUER F H,FEMIANO M D.Attitude control system conceptual design for geostationary operational environmental satellite spacecraft series[J].Journal of Guidance,Control and Dynamics,1995,18(2):247-255.
  • 4LIKINS P W.Dynamics and control of flexible space vehicles[R].JPL,TR-32-1329,1970.
  • 5WILLIAMS C J H.Mathematical methods in flexible spacecraft dynamics[R].ESA,CR(P)-915,1976.
  • 6SUZUKI Y.Acceleration feed forward control for active magnetic bearing systems excited by ground motion[J].IEE Proc.Control Theory Appl.,1998,145(2):113-118.
  • 7KANG M S.Optimal feed forward control of active magnetic bearing system subject to base motion[C].Proceedings of 2003 IEEE Conference on Control Applications,2003,748-753.
  • 8贺泉,韩潮.基于蚁群算法的多任务导航星座载荷配置[J].北京航空航天大学学报,2007,33(10):1154-1157. 被引量:3
  • 9WANG Y,CAI Z X.Combining multiobjective optimization with differential evolution to solve constrained optimization problems [J].IEEE Transactions on Evolutionary Computation,2012,16(1):117-134.
  • 10ZHANG Q F,LI H.MOEA/D:a multi-objective evolutionary algorithm based on decomposition [J].IEEE Transactions on Evolutionary Computation,2007,1(6):712-731.

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