Technical Papers
Aug 13, 2015

State Prediction Model Using Starlight Doppler for Orbital Maneuver and Its Application in XNAV

Publication: Journal of Aerospace Engineering
Volume 29, Issue 2

Abstract

During maneuvering flight, a spacecraft is subject to the engine thrust besides the gravitational force fields of celestial bodies. Moreover, the engine thrust model can hardly be built accurately due to its imbalance. Accordingly, the traditional orbit dynamic mode cannot predict the state accurately, which results in a great decline of navigation filter performance. In order to solve this problem, a state prediction model based on starlight Doppler is proposed for orbital maneuver. In this model, the velocity of the spacecraft is obtained from the starlight Doppler measurement instead of the orbit dynamic model. According to the measured velocities and the constant acceleration model, the state in the navigation filter can be predicted precisely. By this means, the state prediction is not influenced by engine thrust. The proposed state prediction model is applied in the XNAV (X-ray pulsar navigation) system for orbital maneuver. In this navigation system, the starlight Doppler velocity and the pulse time-of-arrival from the X-ray pulsar are utilized to predict and update the state, respectively. The simulation results demonstrate that the state provided by the starlight Doppler-based state prediction model is immune to the engine thrust. The starlight Doppler prediction-based XNAV can provide highly-accurate navigation information for spacecraft orbital maneuvers.

Get full access to this article

View all available purchase options and get full access to this article.

Acknowledgments

This work was supported by the State Key Program of National Natural Science of China (Grant Number 61233005), Specialized Research Fund for the Doctoral Program of Higher Education (Grant Number 20124219120002), Natural Science Foundation of Hubei Province of China (Grant Number 2013CFB333), and National Basic Research Program of China (Grant Number 2014CB744202).

References

Bucy, R. S., and Renne, K. D. (1971). “Digital synthesis of nonlinear filter.” Automatica, 7(3), 287–298.
Buist, P. J., Engelen, S., Noroozi, A., Sundaramoorthy, P., Verhagen, S., and Verhoeven, C. (2011). “Overview of pulsar navigation: Past, present and future trends.” J. Inst. Navig., 58(2), 153–164.
Chester, T. J., and Butman, S. A. (1981). “Navigation using X-ray pulsars.”, Jet Propulsion Laboratory, Pasadena, CA.
Dennis, W. W. (2005). “The use of X-ray pulsars for aiding GPS satellite orbit determination.” Masters dissertation, Air Force Institute of Technology, OH.
Emadzadeh, A. A., and Speyer, J. L. (2011). “X-ray pulsar-based relative navigation using epoch folding.” IEEE Trans. Aerosp. Electron. Syst., 47(4), 2317–2328.
Goshen-Meshin, D. and Bar-Itzhack, I. Y. (1992). “Observability analysis of piece-wise constant system. Part I: Theory.” IEEE Trans. Aerosp. Electron. Syst., 28(4), 1056–1067.
Guo, Y. (1999). “Self-contained autonomous navigation system for deep space mission.” Adv. Astron. Sci., 102(2), 1099–1113.
Kang, X. W., Chen, P., Dong, L. L., and Min, G. R. (2009). “Robust attitude control of flexible liquid spacecraft under fast orbit transfer.” J. Astronaut., 30(4), 1510–1515.
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 Aerosp. Electron. Syst., 30(3), 30–39.
Liu, J., Fang, J. C., Ning, X. L., Wu, J., and Kang, Z. W. (2014). “Closed-loop EKF-based pulsar navigation for Mars explorer with Doppler effects.” J. Navig., 67(5), 775–790.
Liu, J., Kang, Z. W., White, P., Ma, J., and Tian, J. W. (2011). “Doppler/XNAV-integrated navigation system using small-area X-ray sensor.” IET Radar Sonar Navig., 5(9), 1010–1017.
Liu, J., Ma, J., and Tian, J. W. (2010). “CNS/pulsar integrated navigation using two-level filter.” Chin. J. Electron., 19(2), 265–269.
Ma, X., Ning, X. L., and Fang, J. C. (2012). “Analysis of orbital dynamic equation in navigation for a Mars gravity-assist mission.” J. Navig., 65(03), 531–548.
Ning, X. L., Ma, X., Peng, C., Quan, W., and Fang, J. C. (2012). “Analysis of filtering methods for satellite autonomous orbit determination using celestial and geomagnetic measurement.” Math. Prob. Eng., 2012(1), 267875.
Ning, X. L., Wang, L. H, Wu, W. R., and Fang, J. C. (2011). “A celestial assisted INS initialization method for lunar explorers.” Sensors, 11(12), 6991–7003.
Riedel, J. E., Bhaskaran, S., Desai, S., Han, D., Kennedy, B., and Ryne, M. (2000). “Autonomous optical navigation (AutoNav) DS1 technology validation report.” California Institute of Technology, 10.
Satellite Tool Kit version 8.1 [Computer software]. Exton, PA, Analytical Graphics.
Sheikh, S. I., Pines, D. J., and Ray, P. S. (2006). “Spacecraft navigation using X-ray pulsars.” J. Guidance Control Dyn., 29(1), 49–63.
Simon, D. (2006). Optimal state estimation: Kalman, H, and nonlinear approaches, Wiley, New York.
Smith, R. S., and Hadaegh, F. Y. (2005). “Control of deep-space formation-flying spacecraft; relative sensing and switched information.” J. Guidance Control Dyn., 28(1), 106–114.
Sunahara, Y. (1970). “An approximate method of state estimation for nonlinear dynamical systems.” Trans. ASME Ser. D. J. Basic Eng., 92(2), 385–393.
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.” Adv. Space Res., 51(12), 2394–2404.
Xiong, K., Wei, C. L., and Liu, L. D. (2009). “The use of X-ray pulsars for aiding navigation of satellites in constellations.” Acta Astronautica, 64(4), 427–436.
Xu, W. M., Cui, H. T., Cui, P. Y., and Liu, Y. F. (2007). “Selection and planning of asteroids for deep space autonomous optical navigation.” Acta Aeronauticaet Astronautica Sinica, 28(4), 891–896.
Yang, C. W., Deng, X. P., Zheng, J. H., and Gao, D. (2012). “Integrated navigation based on pulsars and sun observation including clock error correction.” J. Beijing Univ. Aeronaut., 38(11), 1469–1473.
Zhang, W., Chen, X., You, W., Zhang, W., and Fang, B. D. (2013). “New autonomous navigation method based on redshift.” Aerosp. Shanghai, 30(2), 32–38.

Information & Authors

Information

Published In

Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 29Issue 2March 2016

History

Received: Dec 18, 2014
Accepted: May 14, 2015
Published online: Aug 13, 2015
Discussion open until: Jan 13, 2016
Published in print: Mar 1, 2016

Permissions

Request permissions for this article.

Authors

Affiliations

Assistant Professor, College of Information Science and Engineering, Wuhan Univ. of Science and Technology, Wuhan 430081, People’s Republic of China; and Postdoctorate, School of Instrumentation Science and Opto-Electronics Engineering, Beihang Univ., Beijing 100191, People’s Republic of China (corresponding author). E-mail: [email protected]
J. C. Fang
Professor, School of Instrumentation Science and Opto-Electronics Engineering, Beihang Univ., Beijing 100191, People’s Republic of China.
Assistant Professor, School of Instrumentation Science and Opto-Electronics Engineering, Beihang Univ., Beijing 100191, People’s Republic of China. E-mail: [email protected]
Z. W. Kang
Professor, College of Information Science and Engineering, Hunan Univ., Changsha 410082, People’s Republic of China.
J. Wu
Professor, College of Information Science and Engineering, Wuhan Univ. of Science and Technology, Wuhan 430081, People’s Republic of China.

Metrics & Citations

Metrics

Citations

Download citation

If you have the appropriate software installed, you can download article citation data to the citation manager of your choice. Simply select your manager software from the list below and click Download.

Cited by

View Options

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Get Access

Access content

Please select your options to get access

Log in/Register Log in via your institution (Shibboleth)
ASCE Members: Please log in to see member pricing

Purchase

Save for later Information on ASCE Library Cards
ASCE Library Cards let you download journal articles, proceedings papers, and available book chapters across the entire ASCE Library platform. ASCE Library Cards remain active for 24 months or until all downloads are used. Note: This content will be debited as one download at time of checkout.

Terms of Use: ASCE Library Cards are for individual, personal use only. Reselling, republishing, or forwarding the materials to libraries or reading rooms is prohibited.
ASCE Library Card (5 downloads)
$105.00
Add to cart
ASCE Library Card (20 downloads)
$280.00
Add to cart
Buy Single Article
$35.00
Add to cart

Media

Figures

Other

Tables

Share

Share

Copy the content Link

Share with email

Email a colleague

Share