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2021 | OriginalPaper | Chapter

9. Simulation Verification of Rendezvous and Docking

Authors : Yongchun Xie, Changqing Chen, Tao Liu, Min Wang

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

Publisher: Springer Singapore

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Abstract

Space rendezvous and docking involves 12 degrees of freedom motion. Rendezvous and docking control is a complex, large-scale, and multi-parameter technology.

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previous chapter Method and Scheme Design of Safety for Rendezvous and Docking
next chapter RVD Verification in Orbit Flight
Literature
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Hirsh, R.L., Chua, Z.K., et al.: Developing a prototype ALHAT human system interface for landing. In: Aerospace Conference, 2011 IEEE Bigsky, MT, USA (2011)
2.
Boge, T., Wimmer, T., Ma, O., et al.: EPOS—Using Robotics for RVD simulation of on-orbit servicing missions. In: Toronto: Canada. AIAA Modeling and Simulation Technologies Conference (2010)
3.
Kiyomi, Y., Kuniharu, Y., Koji, Y.: Test facility for rendezvous and docking system. In: Strengthening Cooperation in the 21st Century v.91: advances in the Astronautical Sciences, Marina del Rey, CA (1995)
4.
Shi, L., Guan, Y.X., Wang, J.H., et al.: Ground validation technology of rendezvous and docking. Sci. Sinica Technol. 44(1), 27–33 (2014)CrossRef
Metadata
Title
Simulation Verification of Rendezvous and Docking
Authors
Yongchun Xie
Changqing Chen
Tao Liu
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_9

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