Since 1963
ARTICLE
Spacecraft attitude fault tolerant control based on multi-objective optimization
1
Aerospace Research Institute, Ministry of Science, Research and Technology, Tehran, Iran
2
Sharif University of Technology, Department of Aerospace Engineering, Tehran, Iran
Submission date: 2019-09-08
Final revision date: 2020-01-26
Acceptance date: 2020-03-25
Online publication date: 2020-10-15
Publication date: 2020-10-15
Journal of Theoretical and Applied Mechanics 2020;58(4):983-996
KEYWORDS
TOPICS
ABSTRACT
An active fault tolerant controller is designed for the attitude control of a faulty spacecraft.
Feedback linearization and Lyapunov’s direct method are used to solve angular velocity
equations and to ensure convergence of the system outputs to reference inputs, respectively.
In order to ensure finite time convergence, final time constraints are proposed. Three con-
structive objective functions are considered as performance measures and optimized using
multi-objective optimization. The results show that the outputs converge to the reference
attitudes, even for severe actuator faults/failures.
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| eISSN: | 2543-6309 |
| ISSN: | 1429-2955 |
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