期刊文献+

基于小波分析的目标轨道机动自主检测方法 被引量:4

Autonomic detection method of space target orbit maneuver based on wavelet analysis
下载PDF
导出
摘要 空间目标的轨道机动是与相对距离变化率的突变联系在一起的.测量值是通过星载激光雷达得到的目标的相对距离,特征量是采用微分平滑处理获得的相对距离变化率.由于测量噪声的影响,机动引起的特征量突变被淹没在噪声中.利用小波分析的多尺度分解,就能够把淹没在噪声中的特征量变化揭示出来.为了满足星上自主运算的要求,提出的机动检测方法就是基于对小波分解后信号的处理,通过对相关系数阈值的比较来检测特征量的突变.仿真结果验证了该检测方法的可行性和有效性. The change rate of relative distance is a character signal of orbit maneuver of space target. Relative distance was measured by laser radar, and the change rate of relative distance was calculated by difference of relative distance. The measure noise was enlarged so the character signal was submerged in the noise. The wavelet analysis in differential scale was used to keep track of time and frequency information of the character signal. With the scale zoom out, the true signal was increased and noise was decreased. The existence of orbit maneuver can be judged by wavelet analysis in differential scale. In order to meet the requirements of autonomic computing on the satellite, the detection method applied correlation coefficient threshold to identification of orbit maneuver. The feasibility and effectiveness were verified by computer numerical simulation.
出处 《北京航空航天大学学报》 EI CAS CSCD 北大核心 2008年第3期353-356,共4页 Journal of Beijing University of Aeronautics and Astronautics
关键词 轨道机动 小波分析 相关系数 飞行动力学 orbital transfer wavelet transforms correlation theory flight dynamics
  • 相关文献

参考文献6

二级参考文献11

  • 1肖业伦.航天器飞行动力学原理[M].北京:宇航出版社,1995..
  • 2张守信.外弹道测量与卫星轨道测量基础[M].北京:国防工业出版社,1992..
  • 3杨福生.小波变换的工程分析与应用[M].北京:科学出版社,2001..
  • 4Allen R.Toso.System-Level Feasibility Analysis of A Microsatellite Rendezvous with Non-cooperative Target[D].Air Force Institute of Technology.2004.
  • 5Thomas M.Davis,Major Tammy L.Baker,Timothy A.Belchak,William R.Larsen.XSS-10 Micro-Satellite Flight Demonstration Program[C].SSC03-1-Ⅳ-1,17th Annual AIAA/USU Conference on Small Satellite.Utah,August 2003.
  • 6Aaron Jacobovits,Thomas W.Vaneck.AeroAstro's Escort-A Microsatellite for On-Orbit Inspection of Space Assets.[C].SSC03-Ⅳ-7,17th Annual AIAA/USU Conference on Small Satellite.Utah,August 2003.
  • 7Battin R.An Introduction to the Mathematics and Methods of Astrodynamics[M].AIAA Education Series,New York,1987.
  • 8Inalhan G,Tillerson M,How J P.Relative Dynamics and Control of Spacecraft Formations in Eccentric Orbits[J].Journal of Guidance,Control and Dynamics,2002,25(1):48 ~59.
  • 9Jinjun Shan,Hong-Tao Liu.Dynamics and Fuzzy Control for Formation Flying with Elliptical Reference Orbits[J].AIAA Guidance,Navigation,and Control Conference and Exhibit,16-19 August 2004,Providence,Rhode Island.AIAA-2004-5025.
  • 10程耕国,周凤星.一种基于小波分析的故障检测与诊断[J].控制与决策,2001,16(B11):828-830. 被引量:19

共引文献96

同被引文献23

引证文献4

二级引证文献7

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