|
- 2018
空间碎片轨道协方差传播及其动态校正
|
Abstract:
轨道误差传播研究在空间碰撞风险分析、任务规划等空间态势感知领域具有重要作用。轨道误差常用误差协方差矩阵表达,其传播方式主要有线性传播模型与非线性传播模型两种。线性传播模型通过状态转移矩阵外推初始协方差矩阵,计算快速,但因将高度非线性化的轨道动力学问题线性化描述,导致传播精度随时间快速降低。非线性传播模型精度高但计算慢,难以进行大规模碎片群的轨道误差传播。在轨道误差传播特性分析的基础上,提出了一种获得较为真实的空间碎片轨道预报误差的方法,分3步进行:初始协方差矩阵的构建、初始轨道协方差线性传播以及基于实测数据对轨道预报协方差的动态校正。经大量案例统计分析,结果表明,校正后的轨道预报协方差,相较于线性传播结果,精度提高了60%以上,可服务于空间碰撞风险分析等高精度空间任务
[1] | Bryan C. International Space Station Debris Avoi-dance Process[J]. NASA Orbital Debris Quarterly News, 2016,20(4):7-8 |
[2] | Chen Lei, Han Lei, Bai Xianzong, et al. Orbital Dynamics and Error Analysis of Space Objects[M]. Beijing:National Defense Industry Press, 2010(陈磊,韩蕾,白显宗,等.空间目标轨道力学与误差分析[M]. 北京:国防工业出版社, 2010) |
[3] | Sabol C, Hill K, Alfriend K, et al. Nonlinear Effects in the Correlation of Tracks and Covariance Propagation[J]. Acta Astronaut, 2013, 84:69-80 |
[4] | NASA Orbital Debris Quarterly News. Satellite Collision Leaves Significant Debris Clouds[OL]. https://orbitaldebris.jsc.nasa.gov/quarterly-news/pdfs/odqnv13i2.pdf, 2018 |
[5] | Li Ming, Gong Zizheng, Liu Guoqing. Frontier Techno-logy and System Development of Space Debris Surveillance and Active Removal[J].Chinese Science Bulletin, 2017, doi:10.1360/N972017-00880(李明,龚自正,刘国青.空间碎片监测移除前沿技术与系统发展[J].科学通报,2017, doi:10.1360/N972017-00880) |
[6] | Bai Xianzong. Research on Orbital Prediction Error and Collision Probablity of Space Objects[D]. Changsha:National University of Defense Techno-logy, 2008(白显宗.空间目标碰撞预警中的碰撞概率问题研究[D].长沙:国防科学技术大学, 2008) |
[7] | Sang J, Bennett J C. Achievable Debris Orbit Prediction Accuracy Using Laser Ranging Data from a Single Station[J]. Advances in Space Research, 2014, 54(1):119-124 |
[8] | Montenbruck O, Gill E. Satellite Orbits:Models, Methods, and Applications[M]. New York:Springer Science & Business Media, 2000 |
[9] | NASA Orbital Debris Quarterly News. Satellite Box Score[OL]. https://orbitaldebris.jsc.nasa.gov/quarterly-news/pdfs/odqnv22i2.pdf, 2018 |
[10] | Luo Y Z, Yang Z. A Review of Uncertainty Propagation in Orbital Mechanics[J]. Progress in Aerospace Science, 2017, 89:23-39 |
[11] | Hoots F R, Roehrich R L. Spacetrack Report No.3-Models for Propagation of NORAD Element Sets[R]. US:US Aerospace Defense Command,1980 |
[12] | Li Bin. Researches on Key Technologies of Fast and Accurate Orbit Determination and Prediction of Space Debris[D]. Wuhan:Wuhan University, 2017(李彬.空间碎片快速精密轨道确定与预报若干关键问题研究[D]. 武汉:武汉大学, 2017) |