Optimal lQR controller design for wing rock motion control in delta wing aircraft
Author
Source
Engineering and Technology Journal
Issue
Vol. 35, Issue 5A (31 May. 2017), pp.473-478, 6 p.
Publisher
Publication Date
2017-05-31
Country of Publication
Iraq
No. of Pages
6
Main Subjects
Engineering & Technology Sciences (Multidisciplinary)
Abstract EN
In this work, an Optimal Linear Quadratic (LQR) and optimal Minimax controller is proposed for Wing Rock Motion Control in Delta wing Aircraft model.
The nonlinear Wing Rock Motion dynamics were considered.
The LQR and Minimax controllers are designed in order to reduce the Wing Rock Motion.
Simulations are performed in order to verify the ability of both controllers to reduce the wing rock motion in delta wing aircraft.
Results were plotted together in order to show the difference of performance for both controllers for a comparative point of view.
American Psychological Association (APA)
Midhat, Bashshar Fatih. 2017. Optimal lQR controller design for wing rock motion control in delta wing aircraft. Engineering and Technology Journal،Vol. 35, no. 5A, pp.473-478.
https://search.emarefa.net/detail/BIM-796475
Modern Language Association (MLA)
Midhat, Bashshar Fatih. Optimal lQR controller design for wing rock motion control in delta wing aircraft. Engineering and Technology Journal Vol. 35, no. 5A (2017), pp.473-478.
https://search.emarefa.net/detail/BIM-796475
American Medical Association (AMA)
Midhat, Bashshar Fatih. Optimal lQR controller design for wing rock motion control in delta wing aircraft. Engineering and Technology Journal. 2017. Vol. 35, no. 5A, pp.473-478.
https://search.emarefa.net/detail/BIM-796475
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references : p. 478
Record ID
BIM-796475