Abstract
The OTV fulfills orbital maneuver by selecting appropriate transfer points to save fuels. Usually, before the orbital maneuver, it shall carry out non-powered free sliding in large elliptic orbit for a long time. During such process, due to the longer sliding period, the error of inertial navigation will be accumulated as time elapses. Meanwhile, when the orbit arrives at a certain height, the availability of satellite navigation signals becomes poor, the flight vehicle could not obtain accurate position and velocity with the INS/GNSS-integrated navigation in real time.
This is a preview of subscription content, log in via an institution.
Buying options
Tax calculation will be finalised at checkout
Purchases are for personal use only
Learn about institutional subscriptionsReference Documentation
Dong, Zezheng. 2010. Research on Mixed Model Orbit Prediction Method Based on Neural Networks. Nanjing University of Aeronautics and Astronautics.
Jingshi, Tang, and Liu Lin. 2014. Preliminary Investigation on Long Term Orbit Prediction of Low Orbit Spacecraft. Journal of Flight Control 33 (1): 59–64.
Liu, Bing. 2006. Research on Orbit Prediction of Lunar Spacecraft. National University of Defense Technology.
Liu, Yifan. 2009. Research on Low-orbit Spacecraft Orbit Prediction Method Based on SGP4 Model. Harbin Institute of Technology.
Liu, Weiping. 2011. Research on Fast Orbit Determination and Prediction Method of Navigation Satellite. The PLA Information Engineering University.
Shi, Li., Zhang, Shijie., and Ye Song, et al. 2010. Design of Elliptical Satellite Orbit Prediction System. Aerospace Control 28 (6): 43–48, 55.
Wang, Shi. 2002. Research on Satellite Orbital Control and Orbit Determination Algorithm. National University of Defense Technology.
Zhao, Liping. 2002. Research on Determination of Autonomous Orbit Determination of Near-earth Satellite and The Control System. Northwestern Polytechnical University.
Author information
Authors and Affiliations
Corresponding author
Rights and permissions
Copyright information
© 2018 Springer Nature Singapore Pte Ltd. and National Defense Industry Press, Beijing
About this chapter
Cite this chapter
Li, X., Li, C. (2018). Orbit Prediction Technology. In: Navigation and Guidance of Orbital Transfer Vehicle. Navigation: Science and Technology. Springer, Singapore. https://doi.org/10.1007/978-981-10-6334-3_3
Download citation
DOI: https://doi.org/10.1007/978-981-10-6334-3_3
Published:
Publisher Name: Springer, Singapore
Print ISBN: 978-981-10-6333-6
Online ISBN: 978-981-10-6334-3
eBook Packages: EngineeringEngineering (R0)