期刊文献+

火星探测巡航段与捕获段光学自主导航方案与关键技术 被引量:11

Scheme and Key Technologies of Autonomous Optical Navigation for Mars Exploration in Cruise and Capture Phase
原文传递
导出
摘要 火星探测是国家深空探测重大专项的重要组成部分,无线电导航受通讯延时与天体遮挡等问题的影响,在导航精度和实时性方面存在问题。光学自主导航作为对地面无线电导航的重要辅助,是火星探测任务顺利完成的重要技术支撑。针对火星探测任务,设计了火星探测巡航段与捕获段的导航方案,并对两个阶段中光学自主导航的关键技术进行了总结与研究,为进一步利用深空天体摄影测量的理论与方法深入开展火星探测光学自主导航关键技术的研究提供参考。 Mars exploration is one of the most important major deep space exploration projects.Some problems,such as navigation accuracyandsignal real-time transmission,exist in radio navigation because of the communication latency and occlusion of celestial bodies.Autonomous optical navigation is a key technology for mars exploration and could act as an important auxiliary for radio navigation.This paper focuses on the scheme and key technologies for autonomous optical navigation in mars exploration durling the cruise and capture phase.Firstly,some concept and scheme of autonomous optical navigation have been discussed,in which the optical navigation measurement model has been introduced for defining the relationship between celestialandoptical navigation camera,and the navigation scheme for marsexploration in cruise and capture phase has been formulated too.Secondly,some key technologies focusing on navigation image processing,on-orbit calibration for optical navigation camera and optical autonomous navigation filter design have been fully presented.In further research,these key technologies could take the advantage of the theoretical basis of Deep-space Photogrammetry.
出处 《武汉大学学报(信息科学版)》 EI CSCD 北大核心 2016年第4期434-442,共9页 Geomatics and Information Science of Wuhan University
基金 国家973计划(2014CB744201) 国家自然科学基金(91438111)~~
关键词 火星探测 光学自主导航 导航方案 关键技术 深空天体摄影测量 mars exploration autonomous optical navigation navigation scheme key technologies deep-space photogrammetry
  • 相关文献

参考文献18

  • 1崔平远,徐瑞,朱圣英,赵凡宇.深空探测器自主技术发展现状与趋势[J].航空学报,2014,35(1):13-28. 被引量:57
  • 2王大轶,黄翔宇.深空探测自主导航与控制技术综述[J].空间控制技术与应用,2009,35(3):6-12. 被引量:37
  • 3张伟.深空探测高精度天文测角测速组合自主导航基础研究[R].中华人民共和国科学技术部,2013.
  • 4Joseph E R, Anderew T V, Robert A W, et al. Optical Navigation Plan and Strategy for the Lunar Lander Altair [C]. AIAA Guidance, Navigation, and Control Conference, Toronto, Ontario Canada, 2010.
  • 5Owen Jr, William M. Methods of Optical Naviga- tion[J]. Advances in the Astronautical Sciences, 2011,140:1 635-1 653.
  • 6Lightsey G E, Christian J A. Onboard Image-pro- cessing Algorithm for a Spacecraft Optical Naviga- tion Sensor System[J]. Journal of Spacecraft and Rockets, 2012,49(2) :337-352.
  • 7Giannitrapani A, Ceccarelli N, Scortecci F, et al. Comparison of EKF and UKF for Spacecraft Locali- zation via Angle Measurements[J]. IEEE Transac- tions on Aerospace and Electronic Systems, 2011, 47(1) :75-84.
  • 8Riedel J E, Bhaskaran S, Desai S, et al. Deep Space 1 Technology Validation Report-autonomous Optical Navigation [ R]. JPL Technology Report, 2000,1-39.
  • 9PolJe B, Frapard B, Saint-Pe O, et al. Autonomous On-board Navigation for Interplanetary Missions [J]. Advances in the Astronautical Sciences, 2003, 113:227-293.
  • 10Chausson L, Elavault S. Optical Navigation Per- formance During Interplanetary Cruise [C]. 17th ISSFD, Russia, Moscow, 2003.

二级参考文献116

  • 1王新洲.GPS基线向量网粗差定位试验[J].武汉测绘科技大学学报,1995,20(2):157-162. 被引量:12
  • 2高为广,杨元喜,崔先强,张双成.IMU/GPS组合导航系统自适应Kalman滤波算法[J].武汉大学学报(信息科学版),2006,31(5):466-469. 被引量:40
  • 3张炘中.汉字识别技术[M].北京:清华大学出版社,1992,9..
  • 4Simon H.Adaptive Filter Theory[M].Verlag:Prentice-Hall,1996
  • 5Wan E A,Nelson A T.Kalman Filtering and Neural Networks[M].New York:Wiley Publishing,2001
  • 6Julier S J,Uhmann J K,Durrant H F.A New Approach for Filtering Nonlinear Systems.American Control Conference[C].Seattle,Washington,1995
  • 7Montenbruck O,Gill E.Satellite Orbits:Models,Methods and Applications[M].New York:Springer-Verlag,2000
  • 8Teunissen P J. Quality Control in Integrated Navigation Systems[J]. Aerospace and Electronic Systems Magazine, 1990,5(7): 35-41.
  • 9Hewitson S, Wang J L. GNSS Receiver Autonomous Integrity Monitoring (RAIM) with a Dynamic Model[J]. Journal of Navigation, 2007, 60 (2) 247-263.
  • 10Umar I B, Washington Y O, Shao Junfeng. Integri- ty of an Integrated GPS/INS System in the Presence of Slowly Growing Errors. Part I: A Critical Re- view[J]. GPSSolution, 2007(11) :173-181.

共引文献141

同被引文献141

引证文献11

二级引证文献50

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部