Optics and Precision Engineering, Volume. 18, Issue 2, 397(2010)

Attitude measurement based on multiple plane X-ray pulsar vector observation

LAN Sheng-chang*... YE Dong, LIN Jie, XU Guo-dong and CAO Xing-hui |Show fewer author(s)
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    References(15)

    [1] [1] WANG F, CAO X B, CHEN X Q. Guidance algorithms for the near-distance rendezvous of on-orbit-servicing spacecraft[J]. Transactions of Japan Society for Aeronautical and Space Sciences, 2007,50(167):9-17.

    [4] [4] SHEIKH S I, PINES D J, RAY P S, et al.. Spacecraft navigation using X-ray pulsars[J]. Journal of Guidance Control and Dynamics, 2006,29(1):49-64.

    [5] [5] RAY P S, WOOD K S, FRITZ G, et al.. The USA X-ray timing experiment[C].American Physical Society, Annul Meeting, Albuquerque, New Mexico, USA, 2002:336-345.

    [6] [6] EMADAZAHEA A A, SPEYER J L, HADAEGH F Y. A parametric study of relative navigation using pulsars[C].ION 64rd Annual Meeting, Cambridge, Massachusetts, 2007:454-460.

    [7] [7] EMADAZAHEA A A, SPEYER J L. A study of pulsar signals modeling and time delay estimation for relative navigation of spacecrafts[C].ION 64th Annual Meeting Cambridge, Massachusetts,2007:119-125.

    [8] [8] TAYLOR J H. Millisecond pulsars: nature most stable clocks[J]. IEEE, 1991,79(7):1054-1062.

    [9] [9] RIBA J, SALA J, VAZQUEZ G. Conditional maximum likelihood timing recovery: estimators and bounds[J].IEEE Transactions on Signal Processing, 2001,49(4):835-851.

    [10] [10] ZHANG H,ZHONG J Y,YUAN J H,et al.. Circuit noise effects on star sensor position accuracy [J]. Opt. Precision Eng., 2006,14(6):1052-1056.(in Chinese)

    [11] [11] LIU Y W,CHEN Y Q.Star- sensor measurement model and its application to the spacecraft attitude determination system[J].Journal of Astronautics,2003,24(2):162-168.(in Chinese)

    [12] [12] LIEBE C C. Accuracy performance of star trackers-a tutorial [J]. IEEE Trans. on Aerospace and Electronics Systems,2002,38(2):587-599.

    [13] [13] ASHBY N, GOLSHAN A R. Minimum uncertainties in position and velocity determination using x-ray photons from millisecond pulsars[C].ION New Technology Meeting,2008, San Diego, CA.

    [14] [14] SALA J, URRUELA A, VILLARES X, et al.. Feasibility Study for a spacecraft navigation system relying on Pulsar Timing Information[R]. ESA Spain,2004.

    [15] [15] SUN Z W, GENG Y H, XU G D, et al.. The combined control algorithm for large angle maneuver of HITSAT-1 small satellite. [J]. Acta Astronautica, 2003,53(6):463-469.

    CLP Journals

    [1] XU Guo-dong, SONG Jia-ning, LI Peng-fei. Pulsar navigation adaptive filtering algorithm based on information quality[J]. Optics and Precision Engineering, 2015, 23(3): 827

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    LAN Sheng-chang, YE Dong, LIN Jie, XU Guo-dong, CAO Xing-hui. Attitude measurement based on multiple plane X-ray pulsar vector observation[J]. Optics and Precision Engineering, 2010, 18(2): 397

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    Paper Information

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    Received: Jul. 7, 2009

    Accepted: --

    Published Online: Aug. 31, 2010

    The Author Email: Sheng-chang LAN (lansc1015@gmail.com)

    DOI:

    CSTR:32186.14.

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