基于漫反射激光测距的火箭残骸翻滚姿态估算
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  • 英文篇名:Tumbling Motion Estimation of Rocket Body Based on Diffuse Reflection Laser Ranging
  • 作者:刘通 ; 沈鸣 ; 高鹏骐 ; 赵有
  • 英文作者:Liu Tong;Shen Ming;Gao Pengqi;ZhaoYou;National Astronomical Observatories,Chinese Academy of Sciences;University of Chinese Academy of Sciences;
  • 关键词:测量 ; 翻滚运动 ; 仿真 ; 火箭残骸 ; 漫反射 ; 激光测距 ; Lomb-Scargle算法
  • 英文关键词:measurement;;tumbling motion;;simulation;;rocket body;;diffuse reflection;;laser ranging;;Lomb-Scargle algorithm
  • 中文刊名:JJZZ
  • 英文刊名:Chinese Journal of Lasers
  • 机构:中国科学院国家天文台;中国科学院大学;
  • 出版日期:2018-10-20 12:03
  • 出版单位:中国激光
  • 年:2019
  • 期:v.46;No.505
  • 基金:国家重大科研装备研制项目(ZDYZ2013-2);; 中国科学院国际合作局对外合作重点项目(181811KYSB20170018)
  • 语种:中文;
  • 页:JJZZ201901027
  • 页数:8
  • CN:01
  • ISSN:31-1339/TN
  • 分类号:219-226
摘要
提出了基于漫反射激光测距数据估算火箭残骸质心位置和翻滚姿态的方法。分析了火箭残骸的翻滚运动,建立了漫反射激光测距仿真模型,详细介绍了估算火箭残骸翻滚轴指向和翻滚周期的理论和仿真方法。采用快速Lomb-Scargle算法对德国Wettzell站测得的Soyuz火箭末级残骸的实测数据进行了分析,通过比较仿真和实测数据的统计直方图,推算了火箭残骸的长度及质心位置,估算得到其观测周期为11.4s,赤经为203°,赤纬为23°。
        A method is proposed to estimate the mass centre position and tumbling motion of rocket body using diffuse reflection laser ranging data.The tumbling motion of rocket body is analysed and the diffuse reflection laser ranging model is built.The theoretical and simulation methods are presented to estimate the tumbling axis orientation and tumbling period of rocket body.The laser ranging data of last stage Soyuz rocket body measured at Wettzell station are processed with the fast Lomb-Scargle algorithm.The length and mass centre position of rocket body are deduced by comparing the histograms of simulated and measured data.The tumbling period is estimated to be 11.4 s,the right ascension is 203°,and the declination is 23°.
引文
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