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Stability Analysis of a Helicopter with an External Slung Load System
Author
Source
Journal of Control Science and Engineering
Issue
Vol. 2016, Issue 2016 (31 Dec. 2016), pp.1-14, 14 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2016-06-05
Country of Publication
Egypt
No. of Pages
14
Main Subjects
Electronic engineering
Information Technology and Computer Science
Abstract EN
This paper describes the stability analysis of a helicopter with an underslung external load system.
The Lyapunov second method is considered for the stability analysis.
The system is considered as a cascade connection of uncertain nonlinear system.
The stability analysis is conducted to ensure the stabilisation of the helicopter system and the positioning of the underslung load at hover condition.
Stability analysis and numerical results proved that if desired condition for the stability is met, then it is possible to locate the load at the specified position or its neighbourhood.
American Psychological Association (APA)
Thanapalan, Kary. 2016. Stability Analysis of a Helicopter with an External Slung Load System. Journal of Control Science and Engineering،Vol. 2016, no. 2016, pp.1-14.
https://search.emarefa.net/detail/BIM-1107894
Modern Language Association (MLA)
Thanapalan, Kary. Stability Analysis of a Helicopter with an External Slung Load System. Journal of Control Science and Engineering No. 2016 (2016), pp.1-14.
https://search.emarefa.net/detail/BIM-1107894
American Medical Association (AMA)
Thanapalan, Kary. Stability Analysis of a Helicopter with an External Slung Load System. Journal of Control Science and Engineering. 2016. Vol. 2016, no. 2016, pp.1-14.
https://search.emarefa.net/detail/BIM-1107894
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1107894