Hostname: page-component-78c5997874-s2hrs Total loading time: 0 Render date: 2024-11-11T02:16:03.423Z Has data issue: false hasContentIssue false

X-ray Pulsar/Starlight Doppler Deeply-integrated Navigation Method

Published online by Cambridge University Press:  09 March 2017

Yidi Wang*
Affiliation:
(College of Aerospace Science and Engineering, National University of Defence Technology, Changsha, China)
Wei Zheng
Affiliation:
(College of Aerospace Science and Engineering, National University of Defence Technology, Changsha, China)
Dapeng Zhang
Affiliation:
(College of Aerospace Science and Engineering, National University of Defence Technology, Changsha, China)

Abstract

An X-ray pulsar/starlight Doppler deeply-integrated navigation method is proposed in this paper. A starlight Doppler measurement-aided phase propagation model, which can remove the orbital effect within the recorded photon Time Of Arrivals (TOAs), is derived, and guarantees that the pulse phase can be extracted from the converted photon TOAs using computationally efficient methods. Some simulations are performed by a hardware-in-loop system to verify the performance of the integrated pulse phase estimation method as well as of the integrated navigation method. The integrated pulse phase estimation method could achieve an estimation performance similar to the existing method for orbiting vehicles at the cost of much less computational complexity, is capable of handling the signals of millisecond pulsars, and is applicable to various vehicles. In addition, the proposed integrated navigation method could provide reliable positioning results for various vehicles.

Type
Research Article
Copyright
Copyright © Cambridge University Press 2017 

Access options

Get access to the full version of this content by using one of the access options below. (Log in options will check for institutional or personal access. Content may require purchase if you do not have access.)

References

REFERENCES

Becker, W., Werner, M., and Jessner, A. (2013). Autonomous Spacecraft Navigation with Pulsars. arXiv preprint arXiv: 1305.4842.Google Scholar
Emadzadeh, A., and Speyer, J. (2011). Navigation in space by X-ray pulsars, Springer Press.CrossRefGoogle Scholar
Emadzadeh, A., and Speyer, J. (2010a). On modelling and pulse phase estimation of X-ray pulsars. IEEE transactions on signal processing, 58, 44844495.CrossRefGoogle Scholar
Emadzadeh, A., and Speyer, J. (2010b). X-ray pulsar-based relative navigation using epoch folding. IEEE transactions on Aerospace and electronic systems, 47, 23172328.Google Scholar
Golshan, A., and Sheikh, S. (2007). On pulse phase estimation and tracking of variable celestial X-ray sources. Presented ION 63rd meeting.Google Scholar
Liu, J., Fang, J.C., Ma, X., Kang, Z.W. and Wu, J. (2015). X-ray pulsar/starlight Doppler Integrated Navigation for formation flight with ephemerides errors. IEEE Aerospace and Electronic Systems Magazine, March, 3039.Google Scholar
Lyne, A. and Craham-Smith, F. (2012). Pulsar astronomy, Cambridge University Press.CrossRefGoogle Scholar
Ning, X.L. and Fang, J.C. (2007). An autonomous celestial navigation method for LEO satellite based on unscented Kalman filter and information fusion, Aerospace Science and Technology, 11, 222228.Google Scholar
Rinauro, S., Colonnese, S. and Scarano, G. (2013). Fast near-maximum likelihood phase estimation of X-ray pulsars, Signal Processing, 93, 326331.Google Scholar
Hildebrand, F. (1974), Introduction to numerical analysis, 2nd edition, McGraw-Hill.Google Scholar
Rutledge, R., Fox, D., Kullkarni, S., Jacoby, B., Cognard, I., Backer, D. and Murray, S. (2004). Microsecond timing of PSR B1821-24 with Chandra/HRC-S. Astrophysics Journal, 613, 522531.Google Scholar
Sala, J., Paredes, J., Urruela, A., Estalella, R. and Villares, X. (2004). Feasibility Study for A Spacecraft Navigation System Relying on Pulsar Timing Information. ARIADNA Study 03/4202.Google Scholar
Sheikh, S.I., Pines, D.J., and Ray, P.S. (2006). Spacecraft Navigation using X-ray Pulsars. Journal of Guidance, Control and Dynamics, 29, 4963.CrossRefGoogle Scholar
Tran, N., Renaux, A., Boyer, R., Marcos, S. and Larzabal, P. (2014). Performance bounds for the pulse-phase estimation of X-ray pulsars, IEEE transaction on Aerospace and electronic systems, 50, 786794.Google Scholar
Wang, Y.D. and Zheng, W. (2016). Pulse phase estimation of X-ray pulsar with the aid of vehicle orbital dynamics. Journal of Navigation, 69, 414432.Google Scholar
Wang, Y.D., Zheng, W., Sun, S.M. and Li, L. (2013). X-ray pulsar-based navigation system with the errors in the planetary ephemerides for Earth-orbiting satellite. Advances in Space Research, 51, 23942404.CrossRefGoogle Scholar
Wang, Y.D., Zheng, W., Sun, S.M. and Li, L. (2014). X-ray pulsar-based navigation using time-differenced measurement. Aerospace Science and Technology, 36, 2735.Google Scholar
Winternitz, L.M.B., Hassouneh, M.A. and Mitchell, J.W. (2015). X-ray pulsar navigation algorithms and testbed for SEXTANT, Technical Report to NASA.Google Scholar
Yang, W. B, Li, S.Y. and Li, N. (2014). A switch-mode information fusion filter based on ISRUKF for autonomous navigation of spacecraft, Information Fusion, 18, 3342.Google Scholar
Yim, J. (2002). Autonomous spacecraft orbit navigation. PhD Thesis, Texas A&M University, 2002.Google Scholar