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In-orbit Demonstration of X-Ray Pulsar Navigation with the Insight-HXMT Satellite

Date
2019
Author
Deng, J. K.
Yang, J. W.
Yang, S.
Yang, Y. J.
Zhang, A. M.
Zhang, C. L.
Zhang, C. M.
Zhang, F.
Zhang, H. M.
Zhang, J.
Zhang, Q.
Zhang, T.
Zhang, W.
Zhang, W. C.
Zhang, W. Z.
Zhang, Y.
Zhang, Y. F.
Zhang, Y. J.
Zhang, Z.
Zhang, Z. L.
Zhao, H. S.
Zhao, J. L.
Zhao, X. F.
Zhu, Y.
Zhu, Y. X.
Zou, C. L.
Gungor, C.
Zheng, S. J.
Zhang, S. N.
Lu, F. J.
Wang, W. B.
Gao, Y.
Li, T. P.
Song, L. M.
Ge, M. Y.
Han, D. W.
Chen, Y.
Xu, Y. P.
Cao, X. L.
Liu, C. Z.
Zhang, S.
Qu, J. L.
Chang, Z.
Chen, G.
Chen, L.
Chen, T. X.
Chen, Y. B.
Chen, Y. P.
Cui, W.
Cui, W. W.
Gao, G. H.
Gao, H.
Gao, M.
Gu, Y. D.
Guan, J.
Guo, C. C.
Dong, Y. W.
Du, Y. Y.
Fu, M. X.
Hu, W.
Huang, Y.
Huo, J.
Ji, J. F.
Jia, S. M.
Jiang, L. H.
Jiang, W. C.
Jin, J.
Jin, Y. J.
Li, B.
Li, C. K.
Li, G.
Li, M. S.
Li, W.
Li, X.
Li, X. B.
Li, X. F.
Li, Y. G.
Li, Z. J.
Li, Z. W.
Liang, X. H.
Liao, J. Y.
Liu, G. Q.
Liu, H. W.
Liu, S. Z.
Liu, X. J.
Liu, Y.
Liu, Y. N.
Lu, B.
Lu, X. F.
Luo, T.
Ma, X.
Meng, B.
Nang, Y.
Nie, J. Y.
Ou, G.
Sai, N.
Shang, R. C.
Sun, L.
Tan, Y.
Tao, L.
Tao, W.
Tuo, Y. L.
Wang, G. F.
Wang, J.
Wang, W. S.
Wang, Y. S.
Wen, X. Y.
Wu, B. B.
Wu, M.
Xiao, G. C.
Xiong, S. L.
Xu, H.
Yan, L. L.
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Abstract
In this work, we report the in-orbit demonstration of X-ray pulsar navigation with Insight-Hard X-ray Modulation Telescope (Insight-HXMT) Satellite, which was launched on 2017 June 15. The new pulsar navigation method "Significance Enhancement of Pulse-profile with Orbit-dynamics" is adopted to determine the orbit with observations of only one pulsar. In this test, the Crab pulsar is chosen and observed by Insight-HXMT from 2017 August 31 to September 5. Using the five-day long observation data, the orbit of Insight-HXMT is determined successfully with the three telescopes onboard: High Energy X-ray Telescope, Medium Energy X-ray Telescope, and Low Energy X-ray Telescope, respectively. By combining all the data, the position and velocity of the Insight-HXMT are pinpointed to within 10 km (3 sigma) and 10 m s(-1) (3 sigma), respectively.
URI
http://hdl.handle.net/20.500.12627/23191
https://doi.org/10.3847/1538-4365/ab3718
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Creative Commons Lisansı

İstanbul Üniversitesi Akademik Arşiv Sistemi (ilgili içerikte aksi belirtilmediği sürece) Creative Commons Alıntı-GayriTicari-Türetilemez 4.0 Uluslararası Lisansı ile lisanslanmıştır.

DSpace software copyright © 2002-2016  DuraSpace
Contact Us | Send Feedback
Theme by 
Atmire NV