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基于线性协方差分析的接近天体在轨导航方法研究 被引量:1

On Autonomous Navigation Based on Linear Covariance Analysis for the Approach Phase of Interplanetary Mission
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摘要 针对深空探测接近段自主导航高精度、高可靠性和实时性的要求,提出在轨融合光学测量信息和无线电测量信息的接近段自主导航方法.为选择合适的光学测量信息和无线电信息在轨融合,结合线性协方差分析方法和基于B平面参数的误差分析方法,分析了不同光学观测信息和无线电测量信息在轨融合的导航方案,说明了提出的自主导航方法可有效提高导航精度,并对光学观测信息的选择给出了合理的建议.基于蒙特卡罗打靶的仿真分析验证了所提出分析方法的有效性. Upon the demands of high accuracy,high reliability and real time for interplanetary navigation system,an autonomous navigation method for the approach phase is proposed,which relies on the on-orbit fusion of optical and radio measurements.To choose appropriate optical measurements and radio measurements for on-orbit fusion,the paper,using a linear covariance analysis and an error analysis method based on B-plane parameters,analyzes various autonomous navigation schemes fusing different optical and radio measurements.The result shows that the proposed autonomous navigation method can effectively improve the navigation accuracy.We also give some principles for reasonable selection of optical measurements.Finally,the presented analysis method is verified by the Monte Carlo target practice based simulation.
出处 《空间控制技术与应用》 2013年第2期17-23,共7页 Aerospace Control and Application
基金 国防基础科研资助项目(B0320110004)
关键词 自主导航 线性协方差分析 B平面参数 信息融合 autonomous navigation linear covariance analysis B-plane parameters information fusion
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参考文献10

  • 1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
  • 2Bhaskaran S,Riedel J E,Synnott S P,et al.The deep space 1 autonomous navigation system:a post-flight analysis[C].AIAA/AAS Astrodynamics Specialist Conference,Denver,CO,USA,Aug 2000.
  • 3Ryne M,Jefferson D,Craig D,et al.Ground-based orbit determination for deep impact[C].The 16th Annual AAS/AIAA Space Flight Mechanics Meeting,San Diego,CA,2006.
  • 4黄翔宇,王大轶.基于光学和无线电信息的接近天体在轨导航方法研究[C].全国第十五届空间及运动体控制技术学术会议,长春,2012.
  • 5黄翔宇,崔平远,崔祜涛.深空自主导航系统的可观性分析[J].宇航学报,2006,27(3):332-337. 被引量:29
  • 6Geller D K,Rose M B,Woffinden D C.Event triggers in linear covariance analysis with applications to orbital rendezvous[J].Journal of Guidance Control and Dynamics,2009,32(1):102-111.
  • 7Geller D K.Linear covariance techniques for orbital rendezvous analysis and autonomous onboard mission planning[J].Journal of Guidance Control and Dynamics,2006,29(6):1404-1414.
  • 8Stastny N B,Geller D K.Autonomous optical navigation at Jupiter:a linear covariance analysis[J].Journal of Spacecraft and Rockets,2008,45 (2):290-298.
  • 9Kizner W.A method of describing miss distances for lunar and interplanetary trajectories[R].NASA CR-63483,1959.
  • 10Byron D T,Bob E S,George H B.Statistical orbit determination[M].USA:Elsevier Academic Press,2004,251-261.

二级参考文献4

  • 1Liu P T,Fang H,Li F and Xiao H.State decouple in estimation theory[A].Proceedings-ICASSP,IEEE International Conference on Acoustics,Speech and Signal Processing[C].1995,2024-2027
  • 2Hermann R,Arthur J K.Nonlinear controllability and observability[J].IEEE Transactions on Automatic Control,1977,22(5):728-740.
  • 3Yim J R.Autonomous Spacecraft Orbit Navigation[M].Ph.D Thesis of Texas A&M University,2002:28-32
  • 4Nikos Mastrodemos,Daniel G. Kubitschek,Stephen P. Synnott. Autonomous Navigation for the Deep Impact Mission Encounter with Comet Tempel 1[J] 2005,Space Science Reviews(1-2):95~121

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