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作 者:Jun-Yang Pan Yi Xie
机构地区:[1]School of Astronomy and Space Science, Nanjing University [2]Key Laboratory of Modern Astronomy and Astrophysics, Nanjing University, Ministry of Education
出 处:《Research in Astronomy and Astrophysics》2015年第2期281-292,共12页天文和天体物理学研究(英文版)
基 金:Supported by the National Natural Science Foundation of China
摘 要:With tremendous advances in modem techniques, Einstein's general rela- tivity has become an inevitable part of deep space missions. We investigate the rela- tivistic algorithm for time transfer between the proper time - of the onboard clock and the Geocentric Coordinate Time, which extends some previous works by including the effects of propagation of electromagnetic signals. In order to evaluate the implicit algebraic equations and integrals in the model, we take an analytic approach to work out their approximate values. This analytic model might be used in an onboard com- puter because of its limited capability to perform calculations. Taking an orbiter like Yinghuo-1 as an example, we find that the contributions of the Sun, the ground station and the spacecraft dominate the outcomes of the relativistic corrections to the model.With tremendous advances in modem techniques, Einstein's general rela- tivity has become an inevitable part of deep space missions. We investigate the rela- tivistic algorithm for time transfer between the proper time - of the onboard clock and the Geocentric Coordinate Time, which extends some previous works by including the effects of propagation of electromagnetic signals. In order to evaluate the implicit algebraic equations and integrals in the model, we take an analytic approach to work out their approximate values. This analytic model might be used in an onboard com- puter because of its limited capability to perform calculations. Taking an orbiter like Yinghuo-1 as an example, we find that the contributions of the Sun, the ground station and the spacecraft dominate the outcomes of the relativistic corrections to the model.
关 键 词:reference systems—time—method:analytical—space vehicles
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