An autonomous orbit determination method for MEO&LEO satellite
文献类型：会议论文
| 作者 | Zhang, Hui; Wang, Jin; Yu, GuoBin; Zhong, Jie; Lin, Ling |
| 出版日期 | 2014 |
| 会议名称 | Proceedings of SPIE: 7th International Symposium on Advanced Optical Manufacturing and Testing Technologies: Optical Test and Measurement Technology and Equipment |
| 会议日期 | 2014 |
| 卷号 | 9282 |
| 页码 | 928213 |
| 中文摘要 | A reliable and secure navigation system and assured autonomous capability of satellite are in high demand in case of emergencies in space. This paper introduces a novel autonomous orbit determination method for Middle-Earth-Orbit and Low-Earth-Orbit (MEO&LEO) satellite by observing space objects whose orbits are known. Generally, the geodetic satellites, such as LAGEOS and ETALONS, can be selected as the space objects here. The precision CCD camera on tracking gimbal can make a series of photos of the objects and surrounding stars when MEO&LEO satellite encounters the space objects. Then the information processor processes images and attains sightings and angular observations of space objects. Several clusters of such angular observations are incorporated into a batch least squares filter to obtain an orbit determination solution. This paper describes basic principle and builds integrated mathematical model. The accuracy of this method is analyzed by means of computer simulation. Then a simulant experiment system is built, and the experimental results demonstrate the feasibility and effectiveness of this method. The experimental results show that this method can attain the accuracy of 150 meters with angular observations of 1 arcsecond system error. © 2014 SPIE. |
| 英文摘要 | A reliable and secure navigation system and assured autonomous capability of satellite are in high demand in case of emergencies in space. This paper introduces a novel autonomous orbit determination method for Middle-Earth-Orbit and Low-Earth-Orbit (MEO&LEO) satellite by observing space objects whose orbits are known. Generally, the geodetic satellites, such as LAGEOS and ETALONS, can be selected as the space objects here. The precision CCD camera on tracking gimbal can make a series of photos of the objects and surrounding stars when MEO&LEO satellite encounters the space objects. Then the information processor processes images and attains sightings and angular observations of space objects. Several clusters of such angular observations are incorporated into a batch least squares filter to obtain an orbit determination solution. This paper describes basic principle and builds integrated mathematical model. The accuracy of this method is analyzed by means of computer simulation. Then a simulant experiment system is built, and the experimental results demonstrate the feasibility and effectiveness of this method. The experimental results show that this method can attain the accuracy of 150 meters with angular observations of 1 arcsecond system error. © 2014 SPIE. |
| 收录类别 | EI |
| 学科主题 | CCD cameras - Earth (planet) - Geodetic satellites - Manufacture - Navigation systems - Optical testing - Satellites |
| 语种 | 英语 |
| ISSN号 | 0277786X |
| 源URL | [http://ir.ioe.ac.cn/handle/181551/7711]  |
| 专题 | 光电技术研究所_光电传感技术研究室（六室） |
| 作者单位 | Institute of Optics and Electronics, Chinese Academy of Sciences, Chengdu, China |
| 推荐引用方式 GB/T 7714 | Zhang, Hui,Wang, Jin,Yu, GuoBin,et al. An autonomous orbit determination method for MEO&LEO satellite[C]. 见:Proceedings of SPIE: 7th International Symposium on Advanced Optical Manufacturing and Testing Technologies: Optical Test and Measurement Technology and Equipment. 2014. |
入库方式： OAI收割
来源：光电技术研究所
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