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Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode
Joint Authors
Fathi Jegarkandi, Mohsen
Ashrafifar, Asghar
Mohsenipour, Reza
Source
International Journal of Aerospace Engineering
Issue
Vol. 2015, Issue 2015 (31 Dec. 2015), pp.1-7, 7 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2015-11-17
Country of Publication
Egypt
No. of Pages
7
Abstract EN
A new method of integrated guidance and control for homing missiles with actuator fault against manoeuvring targets is proposed.
Model of the integrated guidance and control system in the pitch plane with actuator fault and some uncertainty is developed.
A control law using combination of adaptive backstepping and sliding mode approaches is designed to achieve interception in the presence of bounded uncertainties and actuator fault.
Simulation results show that new approach has better performance than adaptive backstepping and has good performance in the presence of actuator fault.
American Psychological Association (APA)
Fathi Jegarkandi, Mohsen& Ashrafifar, Asghar& Mohsenipour, Reza. 2015. Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode. International Journal of Aerospace Engineering،Vol. 2015, no. 2015, pp.1-7.
https://search.emarefa.net/detail/BIM-1064501
Modern Language Association (MLA)
Fathi Jegarkandi, Mohsen…[et al.]. Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode. International Journal of Aerospace Engineering No. 2015 (2015), pp.1-7.
https://search.emarefa.net/detail/BIM-1064501
American Medical Association (AMA)
Fathi Jegarkandi, Mohsen& Ashrafifar, Asghar& Mohsenipour, Reza. Adaptive Integrated Guidance and Fault Tolerant Control Using Backstepping and Sliding Mode. International Journal of Aerospace Engineering. 2015. Vol. 2015, no. 2015, pp.1-7.
https://search.emarefa.net/detail/BIM-1064501
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1064501