![](/images/graphics-bg.png)
Adaptive Fixed-Time Terminal Sliding Mode Control on SE(3) for Coupled Spacecraft Tracking Maneuver
Joint Authors
Wang, Yong
Liao, Ying
Gong, Kejie
Source
International Journal of Aerospace Engineering
Issue
Vol. 2020, Issue 2020 (31 Dec. 2020), pp.1-15, 15 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2020-02-04
Country of Publication
Egypt
No. of Pages
15
Abstract EN
In this paper, a reaching law-based adaptive fixed-time terminal sliding mode control law, which is used for coupled spacecraft tracking maneuver in the presence of large inertia parametric uncertainties and external disturbances, is proposed.
The coupled 6-DOF kinematics and dynamics for spacecraft motion are modeled on Lie group SE(3).
The relative configuration is expressed by a local coordinate (exponential coordinate) of SE(3).
In order to estimate the inertia parameters and external disturbances, we also propose a novel adaptive update law, which can make the control law be applied without the inertia parameters of the spacecraft a priori.
Fixed-time convergence property of the closed-loop feedback system is proved in the framework of Lyapunov.
Numerical simulations are performed to demonstrate the performances of the proposed control scheme for coupled spacecraft tracking maneuver.
American Psychological Association (APA)
Gong, Kejie& Liao, Ying& Wang, Yong. 2020. Adaptive Fixed-Time Terminal Sliding Mode Control on SE(3) for Coupled Spacecraft Tracking Maneuver. International Journal of Aerospace Engineering،Vol. 2020, no. 2020, pp.1-15.
https://search.emarefa.net/detail/BIM-1168021
Modern Language Association (MLA)
Gong, Kejie…[et al.]. Adaptive Fixed-Time Terminal Sliding Mode Control on SE(3) for Coupled Spacecraft Tracking Maneuver. International Journal of Aerospace Engineering No. 2020 (2020), pp.1-15.
https://search.emarefa.net/detail/BIM-1168021
American Medical Association (AMA)
Gong, Kejie& Liao, Ying& Wang, Yong. Adaptive Fixed-Time Terminal Sliding Mode Control on SE(3) for Coupled Spacecraft Tracking Maneuver. International Journal of Aerospace Engineering. 2020. Vol. 2020, no. 2020, pp.1-15.
https://search.emarefa.net/detail/BIM-1168021
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1168021