Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite
Joint Authors
Ni, Jianfei
Huo, Mingyi
Huo, Xing
Karimi, Hamid Reza
Source
Issue
Vol. 2014, Issue 2014 (31 Dec. 2014), pp.1-15, 15 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2014-02-26
Country of Publication
Egypt
No. of Pages
15
Main Subjects
Abstract EN
The problem of finite-time control for attitude tracking maneuver of a rigid spacecraft is investigated.
External disturbance, unknown inertia parameters are addressed.
As stepping stone, a sliding mode controller is designed.
It requires the upper bound of the lumped uncertainty including disturbance and inertia matrix.
However, this upper bound may not be easily obtained.
Therefore, an adaptive sliding mode control law is then proposed to release that drawback.
Adaptive technique is applied to estimate that bound.
It is proved that the closed-loop attitude tracking system is finite-time stable.
The tracking errors of the attitude and the angular velocity are asymptotically stabilized.
Moreover, the upper bound on the lumped uncertainty can be exactly estimated in finite time.
The attitude tracking performance with application of the control scheme is evaluated through a numerical example.
American Psychological Association (APA)
Huo, Mingyi& Huo, Xing& Karimi, Hamid Reza& Ni, Jianfei. 2014. Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite. Abstract and Applied Analysis،Vol. 2014, no. 2014, pp.1-15.
https://search.emarefa.net/detail/BIM-1033668
Modern Language Association (MLA)
Huo, Mingyi…[et al.]. Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite. Abstract and Applied Analysis No. 2014 (2014), pp.1-15.
https://search.emarefa.net/detail/BIM-1033668
American Medical Association (AMA)
Huo, Mingyi& Huo, Xing& Karimi, Hamid Reza& Ni, Jianfei. Finite-Time Control for Attitude Tracking Maneuver of Rigid Satellite. Abstract and Applied Analysis. 2014. Vol. 2014, no. 2014, pp.1-15.
https://search.emarefa.net/detail/BIM-1033668
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1033668