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2021 | OriginalPaper | Chapter

10. RVD Verification in Orbit Flight

Authors : Yongchun Xie, Assoc. Prof. Changqing Chen, Assoc. Prof. Tao Liu, Assoc. Prof. Min Wang

Published in: Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods

Publisher: Springer Singapore

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Abstract

China began to research and develop space RVD technology at the end of the 20th century. After more than ten years of basic theoretical analysis and engineering design research, a series of breakthroughs have been achieved.

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previous chapter Simulation Verification of Rendezvous and Docking
Literature
1.
Xie, Y.C., Zhang, H., Hu, J.: Design of Automatic control system for rendezvous and docking of Shenzhou spacecraft. Sci. China (Technol. Sci.) 44(1), 12–19 (2014)
2.
Hu, J., Xie, Y.C., Zhang, H.: Shenzhou-8 spacecraft rendezvous and docking guidance, navigation and control system and its flight results evaluation. Aerosp. Control Appl. (6), 1–5 (2011)
3.
Hu, H., Xie, Y.C., Hu, J.: Design of the manual control system for the spacecraft rendezvous and docking. Sci. China (Technol. Sci.) 44(1), 34–40 (2014)
4.
Hu, H., Xie, Y.C.: Study on the control method of manual control rendezvous and docking. Chinese Space Sci. Technol. 26(5), 10–16 (2006)
5.
Hu, H., Xie, Y.C.: Research and analysis on manual control rendezvous and docking system of spacecraft in Foreign countries. Control Eng. (1), 21–25 (2005)
Metadata
Title
RVD Verification in Orbit Flight
Authors
Yongchun Xie
Assoc. Prof. Changqing Chen
Assoc. Prof. Tao Liu
Assoc. Prof. Min Wang
Copyright Year
2021
Publisher
Springer Singapore
Book
Guidance, Navigation, and Control for Spacecraft Rendezvous and Docking: Theory and Methods

Print ISBN: 978-981-15-6989-0

Electronic ISBN: 978-981-15-6990-6

Copyright Year: 2021

DOI
https://doi.org/10.1007/978-981-15-6990-6_10

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