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The transformation between τ and TCB for deep space missions under IAU resolutions

The transformation between τ and TCB for deep space missions under IAU resolutions

作     者:Xue-Mei Deng 

作者机构:Purple Mountain Observatory Chinese Academy of Sciences Nanjing 210008 China 

出 版 物:《Research in Astronomy and Astrophysics》 (天文和天体物理学研究(英文版))

年 卷 期:2012年第12卷第6期

页      面:703-712页

核心收录:

学科分类:07[理学] 070102[理学-计算数学] 0704[理学-天文学] 0701[理学-数学] 

基  金:funded by the National Natural Science Foundation of China (Grant Nos. 11103085 and 11178006) 

主  题:reference systems    time    method: analytical    method: numerical   space vehicles 

摘      要:For tracking spacecraft and performing radio science, the transformation between the proper time (τ) given by a clock carried onboard a spacecraft and the barycentric coordinate time (TCB) is investigated under IAU resolutions. In order to more clearly demonstrate manifestations of a physical model and improve computa- tional efficiency, an analytic approach is adopted. After numerical verification, it is confirmed that this method is adequate to describe a Mars orbiter during one year, and is particularly good at describing the influence from perturbing bodies. Further analyses demonstrate that there are two main effects in the transformation: the gravi- tational field of the Sun and the velocity of the spacecraft in the barycentric coordinate reference system. The combined contribution of these effects is at the level of a few sub-seconds.

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