| 引用本文: | 易彬,谷德峰,邵凯,等.BDS在低轨卫星编队高精度相对轨道确定上的应用分析.[J].国防科技大学学报,2020,42(4):43-50.[点击复制] |
| YI Bin,GU Defeng,SHAO Kai,et al.Precise relative orbit determination of LEO formation flying using BDS[J].Journal of National University of Defense Technology,2020,42(4):43-50[点击复制] |
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| BDS在低轨卫星编队高精度相对轨道确定上的应用分析 |
| 易彬1,谷德峰2,邵凯1,易东云1 |
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(1. 国防科技大学 文理学院, 湖南 长沙 410073;2. 中山大学 物理与天文学院, 广东 珠海 519082)
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| 摘要: |
| 分析基于北斗卫星导航系统(BeiDou satellite navigation System, BDS)的低轨卫星编队相对轨道确定问题,但由于缺乏实测数据,通过仿真实验展开研究。结果表明,500 km空域平均可视BDS卫星数约为9.7,由于地球静止轨道(GeoStationary earth Orbit,GEO)卫星和倾斜地球同步轨道(Inclined GeoSynchronous earth Orbit,IGSO)卫星的存在,亚太地区的可视BDS卫星数明显偏多。仅考虑观测噪声的影响时,基于BDS的相对定轨精度可达0.74 mm,加入星历误差的影响,对近距离编队系统的相对定轨而言,GEO卫星数米的星历误差可以忽略,但当星间距离增大到约200 km时,GEO卫星单差后的星历误差可达厘米量级,GEO+IGSO+中圆地球轨道(Medium Earth Orbit,MEO)卫星和IGSO+MEO卫星求解的相对轨道精度分别为1.09 mm和0.96 mm,GEO卫星的加入使得精度下降了13.54%。在其余误差得到有效处理后,BDS的相对定轨精度可达亚毫米量级,且无明显区域差异,GEO卫星和IGSO卫星能提高近距离编队系统的全球相对定轨精度,未来BDS将广泛应用于低轨卫星编队相对轨道确定。 |
| 关键词: 北斗卫星导航系统 低轨卫星编队 相对轨道确定 地球静止轨道卫星 倾斜地球同步轨道卫星 |
| DOI：10.11887/j.cn.202004008 |
| 投稿日期：2019-01-08 |
| 基金项目:国家自然科学基金面上基金资助项目(41874028)；国家自然科学基金重大研究计划资助项目(91438202) |
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| Precise relative orbit determination of LEO formation flying using BDS |
| YI Bin1, GU Defeng2, SHAO Kai1, YI Dongyun1 |
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(1. College of Liberal Arts and Sciences, National University of Defense Technology, Changsha 410073, China;2. School of Physics and Astronomy, Sun Yat-sen University, Zhuhai 519082, China)
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| Abstract: |
| The PROD (precise relative orbit determination) for the LEO (low earth orbit) formation-flying satellites based on BDS (BeiDou satellite navigation system) was studied. Due to the lack of experimental data, the simulation method was used. Results show that the average number of visible BDS satellites at altitude of 500 km is about 9.7. Because of the GEO (geostationary earth orbit) satellites and IGSO (inclined geosynchronous earth orbit) satellites, the LEO satellites can observe more BDS satellites over the Asia-Pacific region. When only the observation noise is considered, the accuracy of PROD based on BDS is 0.74 mm. Furthermore, the influence of ephemeris errors is analyzed. For a few kilometres separation of the LEO satellites, the effect of ephemeris errors on PROD could be ignored. However, for a 200 km separation of the LEO satellites, the SD (single difference) ephemeris errors of GEO satellites would be on the order of centimetres. The experimental results show that when IGSO satellites and MEO satellites co-work with GEO satellites, the accuracy decreased from 1.09 mm to 0.96 mm, decreased by 13.54%. Finally, the conclusion is that the accuracy of PROD based on BDS can reach sub-millimeter level after the remaining errors are processed, the differences of the PROD results are not apparent between different regions. When relative position between satellites is only a few kilometres, the GEO satellites and IGSO satellites can improve the accuracy of PROD all over the world. In the future, BDS will be widely used in PROD of LEO satellites. |
| Keywords: BeiDou satellite navigation system low earth orbit formation flying relative orbit determination geostationary earth orbit satellites inclined geosynchronous earth orbit satellites |
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