NAOC Open IR
基于漫反射激光测距的火箭残骸翻滚姿态估算
刘通; 沈鸣; 高鹏骐; 赵有
2019
Source Publication中国激光
ISSN0258-7025
Volume000Issue:001Pages:219
Abstract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°。
Language英语
Document Type期刊论文
Identifierhttp://ir.bao.ac.cn/handle/114a11/37740
Collection中国科学院国家天文台
Affiliation中国科学院国家天文台
First Author AffilicationNational Astronomical Observatories, Chinese Academy of Sciences
Recommended Citation
GB/T 7714
刘通,沈鸣,高鹏骐,等. 基于漫反射激光测距的火箭残骸翻滚姿态估算[J]. 中国激光,2019,000(001):219.
APA 刘通,沈鸣,高鹏骐,&赵有.(2019).基于漫反射激光测距的火箭残骸翻滚姿态估算.中国激光,000(001),219.
MLA 刘通,et al."基于漫反射激光测距的火箭残骸翻滚姿态估算".中国激光 000.001(2019):219.
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