Robust Tracking Control for Rendezvous in Near-Circular Orbits
Joint Authors
Wan, Neng
Liu, Ming
Karimi, Hamid Reza
Source
Mathematical Problems in Engineering
Issue
Vol. 2013, Issue 2013 (31 Dec. 2013), pp.1-11, 11 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2013-12-18
Country of Publication
Egypt
No. of Pages
11
Main Subjects
Abstract EN
This paper investigates a robust guaranteed cost tracking control problem for thrust-limited spacecraft rendezvous in near-circular orbits.
Relative motion model is established based on the two-body problem with noncircularity of the target orbit described as a parameter uncertainty.
A guaranteed cost tracking controller with input saturation is designed via a linear matrix inequality (LMI) method, and sufficient conditions for the existence of the robust tracking controller are derived, which is more concise and less conservative compared with the previous works.
Numerical examples are provided for both time-invariant and time-variant reference signals to illustrate the effectiveness of the proposed control scheme when applied to the terminal rendezvous and other astronautic missions with scheduled states signal.
American Psychological Association (APA)
Wan, Neng& Liu, Ming& Karimi, Hamid Reza. 2013. Robust Tracking Control for Rendezvous in Near-Circular Orbits. Mathematical Problems in Engineering،Vol. 2013, no. 2013, pp.1-11.
https://search.emarefa.net/detail/BIM-1010512
Modern Language Association (MLA)
Wan, Neng…[et al.]. Robust Tracking Control for Rendezvous in Near-Circular Orbits. Mathematical Problems in Engineering No. 2013 (2013), pp.1-11.
https://search.emarefa.net/detail/BIM-1010512
American Medical Association (AMA)
Wan, Neng& Liu, Ming& Karimi, Hamid Reza. Robust Tracking Control for Rendezvous in Near-Circular Orbits. Mathematical Problems in Engineering. 2013. Vol. 2013, no. 2013, pp.1-11.
https://search.emarefa.net/detail/BIM-1010512
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1010512