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Orbit determination using incremental phase and TDOA of X-ray pulsar
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作者 Rong JIAO Lu-ping XU +1 位作者 Hua ZHANG Cong LI 《Frontiers of Information Technology & Electronic Engineering》 SCIE EI CSCD 2016年第6期543-552,共10页
X-ray pulsars offer stable, periodic X-ray pulse sequences that can be used in spacecraft positioning systems. A method using X-ray pulsars to determine the initial orbit of a satellite is presented in this paper. Thi... X-ray pulsars offer stable, periodic X-ray pulse sequences that can be used in spacecraft positioning systems. A method using X-ray pulsars to determine the initial orbit of a satellite is presented in this paper. This method suggests only one detector to be equipped on the satellite and assumes that the detector observes three pulsars in turn. To improve the performance, the use of incremental phase in one observation duration is proposed, and the incremental phase is combined with the time difference of arrival(TDOA). Then, a weighted least squares(WLS) algorithm is formulated to calculate the initial orbit. Numerical simulations are performed to assess the proposed orbit determination method. 展开更多
关键词 Orbit determination algorithm Single X-ray pulsar detector Phase increment Two-body motion equations Weighted least squares method
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