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星间相对状态测量方法综述 被引量:1

The Summary of Measuring Methods for Inter-satellite State
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摘要 空间状态测量是编队卫星应用需要解决的关键技术之一。通过介绍星间相对状态测量的应用背景及国外研究与应用情况,分析了3种主要的测量方法:GNSS相对定位法、微波相对定位法和光电测量法。针对这3种测量方法提出了有关技术的主要研究方向,通过对这3种方法进行综合比较,提出了针对现状的星间相对状态测量初步想法。  Space state measurement is one of the key technologies for the application of formation-flying satellites.This paper introduces the application background of formation-flying satellites and the status of research and application abroad,analyses the three measurements(method on GNSS,method on microwaves and method on optoelectronics),and advances many directions of technical study.Finally,a design is put forward by comparing three methods.
出处 《无线电工程》 2007年第10期53-55,共3页 Radio Engineering
关键词 空间状态测量 编队卫星 全球定位导航系统 微波测量 光电测量 inter-satellite space state measurement formation-flying satellites GNSS microwave measurement photoelectric measurement
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  • 1梁甸农,朱炬波,董臻.小卫星分布式雷达[J].中国基础科学,2004,6(6):7-10. 被引量:9
  • 2Sien-Chong Wu and Da Kuang. Positioning with Autonomous Formation Flyer (AFF) on Space-Technology 3. ION GPS'99,14-17 September 1999,385-392.
  • 3Parkinson B W and Spilker J J Jr. ,eds. Global Positioning System: Theory and Applications. Progress in Astronautics and Aeronautics,American Institute of Aeronautics and stronautics, Inc. , 1996.
  • 4Corazzini T and How J. Onboard GPS Signal Augmentation for Spacecraft Formation Flying. ION GPS'98, Sept 1998,1937-1946.
  • 5Corazzini T and How J. Onboard Pesudolite Augmentation System for Relative Navigation. ION GPS'99,14-17 September 1999,1559-1568.
  • 6Purcell G, Kuang D, Lichten S, Wu S, Young L. Autonomous formation flyer sensor technology development. Paper AAS 98-062, 21st Ann. AAS Guid. Cont. Conf., Breckenridge, 1998. 1--21.
  • 7Park Chan-Woo, How Jonathan P, Capots Larry. Sensing technologies for formation flying spacecraft in LEO using CDGPS and an inter-spacecraft communications system. ION GPS 2000, 2000, Salt Lake City, 1595---1607.
  • 8Wu Sien-Chong, Kuang Da. Positioning with Autonomous Formation Flyer (AFF) on Space-Technology 3. ION GPS'99, 1999, Nashville, 385---392.
  • 9Parkinson B W, Spilker J J Jr et al. Global Positioning System: Theory and Applications. Prog.Astron. Aeron., Amer. Ins. Aeron. Astron., Inc., 1996.
  • 10Olsen E A, Park Chan-Woo, How Jonathan P. Carrier-phase bias initialization for formation flying vehicles with onboard pseudolites. ION GPS'99, 1999, Nashville, 459--468.

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  • 1罗建军,杨宇和,袁建平.共面快速受控绕飞轨迹设计与控制[J].宇航学报,2006,27(6):1389-1392. 被引量:13
  • 2朱彦伟,杨乐平.航天器在轨服务接近策略研究[J].中国空间科学技术,2007,27(1):14-20. 被引量:16
  • 3唐国金,罗亚中.空间交会对接任务规划[M].北京:科学出版社,2007.
  • 4HIROHISA K. Fly-Around Motion Control Based on Ex- act Linearization with Adaptive Law [ J ]. Journal of Guidance, Control and Dynamics. 2005, 28( 1 ) : 167 - 169.
  • 5HARI B H, MYRON T, DAVID D. Guidance Algo- rithms for Autonomous Rendezvous of Spacecraft with a Target Vehicle in Circular Orbit [ C ] // AIAA Guidance, Navigation, and Control Conference and Exhibit. 2001: 1 -15.
  • 6Stanley D Straight. Maneuver Design for Fast Satellite Circumnavigation[ D ]. Captain, USAF : Air Force Insti- tute of Technology, 2004.
  • 7LILLIE C F. On-Orbit Servicing for Futher Space Ob- servatories[ C ] //AIAA Space Conference and Exposi- tion, Long Beach, CA, 2005:1 -11.
  • 8CLOHESSY W H, WILTSHIRE R S. Terminal Guid- ance System for Satellite Rendezvous[ J]. Journal of the Aerospace Sciences, 1960,27 (9) : 653 -658.
  • 9BYUN S H. Satellite Orbit Determination Using Triple- Differenced GPS Carrier Phase in Pure Kinematic Mode [Jl. Journal of Geodesy, 2003,76(9): 569-585.
  • 10赵齐乐,施闯,柳响林,葛茂荣.重力卫星的星载GPS精密定轨[J].武汉大学学报(信息科学版),2008,33(8):810-814. 被引量:20

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