Robust Parametric Control of Spacecraft Rendezvous
Joint Authors
Source
Mathematical Problems in Engineering
Issue
Vol. 2014, Issue 2014 (31 Dec. 2014), pp.1-5, 5 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2014-05-19
Country of Publication
Egypt
No. of Pages
5
Main Subjects
Abstract EN
This paper proposes a method to design the robust parametric control for autonomous rendezvous of spacecrafts with the inertial information with uncertainty.
We consider model uncertainty of traditional C-W equation to formulate the dynamic model of the relative motion.
Based on eigenstructure assignment and model reference theory, a concise control law for spacecraft rendezvous is proposed which could be fixed through solving an optimization problem.
The cost function considers the stabilization of the system and other performances.
Simulation results illustrate the robustness and effectiveness of the proposed control.
American Psychological Association (APA)
Gu, Dake& Liu, Yindong. 2014. Robust Parametric Control of Spacecraft Rendezvous. Mathematical Problems in Engineering،Vol. 2014, no. 2014, pp.1-5.
https://search.emarefa.net/detail/BIM-511671
Modern Language Association (MLA)
Gu, Dake& Liu, Yindong. Robust Parametric Control of Spacecraft Rendezvous. Mathematical Problems in Engineering No. 2014 (2014), pp.1-5.
https://search.emarefa.net/detail/BIM-511671
American Medical Association (AMA)
Gu, Dake& Liu, Yindong. Robust Parametric Control of Spacecraft Rendezvous. Mathematical Problems in Engineering. 2014. Vol. 2014, no. 2014, pp.1-5.
https://search.emarefa.net/detail/BIM-511671
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-511671