Some Discussion on X-Ray Pulsar Navigation in Astrometry
LI Liang1,2, WANG Guangli1,2, GUO Li1,2, HU Xiaogong1,2
Author information+
1. Shanghai Astronomical Observatory,Chinese Academy of Sciences,Shanghai 200030,China; 2. University of Chinese Academy of Sciences,Beijing 100049,China
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History+
Received
Revised
31 May 2018
20 Jul 2018
Issue Date
20 May 2022
Abstract
The X-ray pulsar-based navigation (XNAV) technology is to determine the attitude,position and velocity of spacecraft using X-ray signals emitted from pulsars. The feasibility and sustainability of pulsar navigation is invented through theoretical astrometric analyses. The processing and modeling of pulsar signals of both X-ray and radio band is introduced,and then investigate The key problems in pulsar navigation are analyzed,and finally the applicable range of distance of XNAV is discussed. The our analyses show that the acquiring of the measurements is highly influenced by the spacecraft velocity. With the error of less than 3 m/s,the profile of a pulsar signal can be got,and from which the time of arrival (TOA) could be obtained. Also,the phase cycle ambiguity is a non-negligible problem in pulsar navigation.
LI Liang, WANG Guangli, GUO Li, HU Xiaogong.
Some Discussion on X-Ray Pulsar Navigation in Astrometry. Journal of Deep Space Exploration, 2018, 5(3): 235‒240 https://doi.org/10.15982/j.issn.2095-7777.2018.3.005
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References
[1] ?DOWNS G S. Interplanetary navigation using pulsating radio sources,NASA Technical Reports N74- 34150[R]. USA:NASA,1974:1-12. [2] CHESTER T J,BUTMAN S A. Navigation using X-ray pulsars,NASA Technical Reports 81N27129 [R]. USA:NASA,1981. [3] WOODS K S. Navigation studies utilizing the NRL-801 experiment and the ARGOS satellite[C]//HORAIS B J. Small Satellite Technology and Applications III. International Society of Optical Engineering(SPIE)Proceedings,Optical Engineering and Photonics in Aerospace Sensing. Orlando,FL,United States:SPIE,1993:105-116. [4] HANSON J E. Principles of X-ray navigation[D]. California:Stanford University,1996. [5] SHEIKH S I. The use of variable celestial X-ray sources for spacecraft navigation[D]. Washington:University of Maryland,2005. [6] EMADZADEH A A,SPEYER J L. Navigation in space by X-ray pulsars[M]. USA:Springer Science and Business Media,2011. [7] MITCHELL J W,WINTERNITZ L M,HASSOUNEH,MUNTHER A,et al. SEXTANT X-ray pulsar navigation demonstration:initial on-orbit results[C]//41st Annual American Astronautical Society (AAS) Guidance and Control Conference 2018. Breckenridge,CO,United States:American Astronautical Society,2018. [8] SALA A. Feasibility study for a spacecraft navigation system relying on pulsar timing information,ARIADNA Study 03/4202[R]. [S.l]:European Space Agency Advanced Concepts Team,2004. [9] SHEIKH S I. GOLSHAN A R,PINES D J. Absolute and relative position determination using variable celestial X-ray sources[C]//30th Annual AAS Guidance and Control Conference. Breckenridge,USA:American Astronautical Society,2007.
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