The earth gravity field model CDS01S of degree and order 36 has been recovered from the post processed Science Orbits and on-board accelerometer data of GFZ’s CHAMP satellite. The model resolves the geoid with an acc...The earth gravity field model CDS01S of degree and order 36 has been recovered from the post processed Science Orbits and on-board accelerometer data of GFZ’s CHAMP satellite. The model resolves the geoid with an accuracy of better than 4 cm at a resolution of 700 km half-wavelength. By using the degree difference variances of geopotential coefficients to compare the model CDS01S with EIGEN3P, EIGEN1S and EGM96, the result indicates that the coefficients of CDS01S are most close to those of EIGEN3P. The result of the comparison between the accuracies of geopotential coefficients in the above models, indicates that the accuracy of coefficients in CDS01S is higher than that in EGM96.The geoid undulations of CDS01S and GGM01C up to 30 degrees are calculated and the standard deviation is 4.7 cm between them.展开更多
We use induced orbit covers to define induced orbit data.By studying the space of regular functions on orbit cover,we know that the induced representation has close connection with the induced orbit datum under the me...We use induced orbit covers to define induced orbit data.By studying the space of regular functions on orbit cover,we know that the induced representation has close connection with the induced orbit datum under the meaning of Vogan’s conjecture.Therefore,when verifying Vogan’s conjecture,many cases can be reduced to the case of rigid orbit data.展开更多
提出一种改进的初轨确定算法,基于动态阈值的距离搜索方法,以改进传统算法在处理数据时初轨成功率和初轨误差。通过动态调整搜索阈值,旨在实现更精准和高效的初轨确定,以满足当前对空间目标初轨确定的需求;利用LEO,MEO和GEO目标的实测...提出一种改进的初轨确定算法,基于动态阈值的距离搜索方法,以改进传统算法在处理数据时初轨成功率和初轨误差。通过动态调整搜索阈值,旨在实现更精准和高效的初轨确定,以满足当前对空间目标初轨确定的需求;利用LEO,MEO和GEO目标的实测角度数据开展算法测试。介绍了基于动态阈值的距离搜索算法的实现过程,基于数据处理的经验,用动态阈值实现初轨参数质量控制环节的轨道筛选。给出了详细的算法实现流程。利用TLE(Two Line El⁃ements)评估了初轨确定参数误差。基于“烛龙”观测网的中低轨目标和中国科学院长春人造卫星观测站的高轨目标的实测角度数据,开展算法测试。结果表明:LEO,MEO和GEO目标短弧初轨确定成功率分别约为94%,75%和89%,半长轴误差均值分别约为9,12和50 km。该算法适用性强、成功率高、定轨精度高,证明了监测数据的质量。展开更多
This paper describes the modeling and simulation of the protocol of CCSDS advanced orbiting systems (AOS). The network features modeled in the implementation of CCSDS AOS are to multiplex different kinds of sources in...This paper describes the modeling and simulation of the protocol of CCSDS advanced orbiting systems (AOS). The network features modeled in the implementation of CCSDS AOS are to multiplex different kinds of sources into virtual channel data units ( VCDUs) in the data processing module. The emphasis of this work is placed on the algorithm for com-mutating VCDUs into physical channels in the form of continuous data stream. The objectives of modeling CCSDS AOS protocol are to analyze the performance of this protocol when it is used to process various data.展开更多
A medium earth orbit （MEO） tracking and data relay satellite system （TDRSS） constellation scheme for China is proposed. This system consists of MEO satellite constellation, inter-satellite links （ISLs） and terre...A medium earth orbit （MEO） tracking and data relay satellite system （TDRSS） constellation scheme for China is proposed. This system consists of MEO satellite constellation, inter-satellite links （ISLs） and terrestrial gateway station, which can provide continuous bidirectional data transmission links between low altitude spacecrafls and the terrestrial gateway station in China. Theoretical analysis and simulation results indicate that the proposed constellation can cover the global low altitude space sphere and earth surface of China continuously, and has a preferable practical perspective.展开更多
文摘The earth gravity field model CDS01S of degree and order 36 has been recovered from the post processed Science Orbits and on-board accelerometer data of GFZ’s CHAMP satellite. The model resolves the geoid with an accuracy of better than 4 cm at a resolution of 700 km half-wavelength. By using the degree difference variances of geopotential coefficients to compare the model CDS01S with EIGEN3P, EIGEN1S and EGM96, the result indicates that the coefficients of CDS01S are most close to those of EIGEN3P. The result of the comparison between the accuracies of geopotential coefficients in the above models, indicates that the accuracy of coefficients in CDS01S is higher than that in EGM96.The geoid undulations of CDS01S and GGM01C up to 30 degrees are calculated and the standard deviation is 4.7 cm between them.
基金supported by National Natural Science Foundation of China(Grant No.10971103)
文摘We use induced orbit covers to define induced orbit data.By studying the space of regular functions on orbit cover,we know that the induced representation has close connection with the induced orbit datum under the meaning of Vogan’s conjecture.Therefore,when verifying Vogan’s conjecture,many cases can be reduced to the case of rigid orbit data.
文摘提出一种改进的初轨确定算法,基于动态阈值的距离搜索方法,以改进传统算法在处理数据时初轨成功率和初轨误差。通过动态调整搜索阈值,旨在实现更精准和高效的初轨确定,以满足当前对空间目标初轨确定的需求;利用LEO,MEO和GEO目标的实测角度数据开展算法测试。介绍了基于动态阈值的距离搜索算法的实现过程,基于数据处理的经验,用动态阈值实现初轨参数质量控制环节的轨道筛选。给出了详细的算法实现流程。利用TLE(Two Line El⁃ements)评估了初轨确定参数误差。基于“烛龙”观测网的中低轨目标和中国科学院长春人造卫星观测站的高轨目标的实测角度数据,开展算法测试。结果表明:LEO,MEO和GEO目标短弧初轨确定成功率分别约为94%,75%和89%,半长轴误差均值分别约为9,12和50 km。该算法适用性强、成功率高、定轨精度高,证明了监测数据的质量。
文摘This paper describes the modeling and simulation of the protocol of CCSDS advanced orbiting systems (AOS). The network features modeled in the implementation of CCSDS AOS are to multiplex different kinds of sources into virtual channel data units ( VCDUs) in the data processing module. The emphasis of this work is placed on the algorithm for com-mutating VCDUs into physical channels in the form of continuous data stream. The objectives of modeling CCSDS AOS protocol are to analyze the performance of this protocol when it is used to process various data.
基金National Natural Science Foundation of China (No. 60372013)
文摘A medium earth orbit （MEO） tracking and data relay satellite system （TDRSS） constellation scheme for China is proposed. This system consists of MEO satellite constellation, inter-satellite links （ISLs） and terrestrial gateway station, which can provide continuous bidirectional data transmission links between low altitude spacecrafls and the terrestrial gateway station in China. Theoretical analysis and simulation results indicate that the proposed constellation can cover the global low altitude space sphere and earth surface of China continuously, and has a preferable practical perspective.
