Helicopter Control Energy Reduction Using Moving Horizontal Tail
Joint Authors
Source
Issue
Vol. 2015, Issue 2015 (31 Dec. 2015), pp.1-10, 10 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2015-06-09
Country of Publication
Egypt
No. of Pages
10
Main Subjects
Medicine
Information Technology and Computer Science
Abstract EN
Helicopter moving horizontal tail (i.e., MHT) strategy is applied in order to save helicopter flight control system (i.e., FCS) energy.
For this intention complex, physics-based, control-oriented nonlinear helicopter models are used.
Equations of MHT are integrated into these models and they are together linearized around straight level flight condition.
A specific variance constrained control strategy, namely, output variance constrained Control (i.e., OVC) is utilized for helicopter FCS.
Control energy savings due to this MHT idea with respect to a conventional helicopter are calculated.
Parameters of helicopter FCS and dimensions of MHT are simultaneously optimized using a stochastic optimization method, namely, simultaneous perturbation stochastic approximation (i.e., SPSA).
In order to observe improvement in behaviors of classical controls closed loop analyses are done.
American Psychological Association (APA)
Oktay, Tugrul& Sal, Firat. 2015. Helicopter Control Energy Reduction Using Moving Horizontal Tail. The Scientific World Journal،Vol. 2015, no. 2015, pp.1-10.
https://search.emarefa.net/detail/BIM-1078863
Modern Language Association (MLA)
Oktay, Tugrul& Sal, Firat. Helicopter Control Energy Reduction Using Moving Horizontal Tail. The Scientific World Journal No. 2015 (2015), pp.1-10.
https://search.emarefa.net/detail/BIM-1078863
American Medical Association (AMA)
Oktay, Tugrul& Sal, Firat. Helicopter Control Energy Reduction Using Moving Horizontal Tail. The Scientific World Journal. 2015. Vol. 2015, no. 2015, pp.1-10.
https://search.emarefa.net/detail/BIM-1078863
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1078863