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2021 | OriginalPaper | Chapter

4. Guidance Method and Schematic Design for 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

In Chap. 1, the process of rendezvous and docking of a flight mission is divided into far range rendezvous phase and near range autonomous control phase based on the distance.

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previous chapter Navigation Method and Scheme Design for Rendezvous and Docking
next chapter Automatic Control Method and Scheme Design for Rendezvous and Docking
Literature
1.
Changqing, C.: Trajectory Safety and Optimization of Rendezvous and Docking. Beijing Institute of Control Engineering (2008) (In Chinese)
2.
Prussing, J E.: Optimal Multiple - Impulse Orbital Rendezvous. Sc. D. thesis, Department of Aeronautics and Astronautics Massachusetts Institute of Technology (1967)MathSciNet
3.
Changqing, C, Yongchun X.: Optimal Impulsive Ellipse-to-Circle Coplanar Rendezvous[J]. Science in China (Series E), 52(5), 1135–1143 (2009)MathSciNetCrossRef
4.
Prussing, J E.: Optimal Impulsive Linear Systems: Sufficient Conditions and Maximum Number of Impulse[J]. The Journal of the Astronautical Science, 43(2), 195–206 (1995)
Metadata
Title
Guidance Method and Schematic Design for 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_4

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