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行星际火箭和人造行星卫星的轨道设计问题 被引量:5

THE ORBITS DISIGNING FOR INTERPLANETARY PROBES AND ARTIFICIAL PLANETARY SATELLITES
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摘要 本文探讨行星际探测器和人造行星卫星的动力学模型,研究它们的运动轨道,给出飞行时间的近似式,并且从飞行时间和消耗能量二个方面对它们的轨道设计问题提出了一些新的看法.另外,文中还讨论了人造行星卫星的运动及其稳定条件. In this paper, the dynamical model, orbital motion and mission time for interplanetary probe and artificial planetary satellite are given. The disign for orbit to cut mission time and save fuel is discussed and the stable region of artificial planetary satellite is also obtained.
作者 郑学塘
出处 《空间科学学报》 CAS CSCD 北大核心 1991年第1期40-45,共6页 Chinese Journal of Space Science
基金 国家自然科学基金
关键词 行星探测器 卫星 轨道动力学 设计 Interplanetary probe, Artificial planetary satellitet, Dynamics of orbits
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参考文献4

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  • 4郑学塘,人造地球卫星的运动和预报,1981年

同被引文献10

  • 1刘军,韩潮.基于UKF的雷达高度计自主定轨[J].北京航空航天大学学报,2006,32(8):889-893. 被引量:3
  • 2Sala J, Urruela A, Villares X. Feasibility Study for a Spacecraft Navigation System Relying on Pulsar Timing Information [ M ] . ARIADNA Study 03P4202,2003,6.
  • 3Sheikh S I. The Use of Variable Celestial X-Ray Sources for Spacecraft Navigation [ D ]. Dissertation Submitted to the Faculty of the Graduate School of the University of Maryland, College Park, in Partial Fulfillment of the Requirements for the Degree of Doctor of Philosophy,2005.
  • 4SongTT, NingX L, Yu W B. A New Autonomous Celestial Method for Mars Probe [ J]. Proceedings of SPIE- The International Society for Optical Engineering, v 6357 II, 2006, p 63574N.
  • 5Sheikh S I, Pines D J. Recursive Estimation of Spacecraft Position and Velocity Using X-ray Pulsar Time of Arrival Measurements [J]. Journal of The Institute of Navigation, 2006,53 ( 3 ).
  • 6Sheikh S I. The use of variable celestial X-ray sources for spacecraft navigation[ D]. America: College Park, University of Maryland ,2005.
  • 7Sheikh S I, Pines D J. Recursive estimation of spacecraft position and velocity using X-ray pulsar time of arrival measurements [J]. Navigation, 2006, 53(3): 149-166.
  • 8郑学塘,天体力学和天文动力学,1989年
  • 9Zheng Xuetang,Chin Phys Lett,1993年,10卷,61页
  • 10郑学塘,天体力学和天文动力学,1989年,112页

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