Control System Design for a Ducted-Fan Unmanned Aerial Vehicle Using Linear Quadratic Tracker
Joint Authors
Jeong, Junho
Kim, Seungkeun
Suk, Jinyoung
Source
International Journal of Aerospace Engineering
Issue
Vol. 2015, Issue 2015 (31 Dec. 2015), pp.1-12, 12 p.
Publisher
Hindawi Publishing Corporation
Publication Date
2015-11-18
Country of Publication
Egypt
No. of Pages
12
Abstract EN
Tracking control system based on linear quadratic (LQ) tracker is designed for a ducted-fan unmanned aerial vehicle (UAV) under full flight envelope including hover, transition, and cruise modes.
To design the LQ tracker, a system matrix is augmented with a tracking error term.
Then the control input can be calculated to solve a single Riccati equation, but the steady-state errors might still remain in this control system.
In order to reduce the steady-state errors, a linear quadratic tracker with integrator (LQTI) is designed to add an integral term of tracking state in the state vector.
Then the performance of the proposed controller is verified through waypoint navigation simulation under wind disturbance.
American Psychological Association (APA)
Jeong, Junho& Kim, Seungkeun& Suk, Jinyoung. 2015. Control System Design for a Ducted-Fan Unmanned Aerial Vehicle Using Linear Quadratic Tracker. International Journal of Aerospace Engineering،Vol. 2015, no. 2015, pp.1-12.
https://search.emarefa.net/detail/BIM-1064511
Modern Language Association (MLA)
Jeong, Junho…[et al.]. Control System Design for a Ducted-Fan Unmanned Aerial Vehicle Using Linear Quadratic Tracker. International Journal of Aerospace Engineering No. 2015 (2015), pp.1-12.
https://search.emarefa.net/detail/BIM-1064511
American Medical Association (AMA)
Jeong, Junho& Kim, Seungkeun& Suk, Jinyoung. Control System Design for a Ducted-Fan Unmanned Aerial Vehicle Using Linear Quadratic Tracker. International Journal of Aerospace Engineering. 2015. Vol. 2015, no. 2015, pp.1-12.
https://search.emarefa.net/detail/BIM-1064511
Data Type
Journal Articles
Language
English
Notes
Includes bibliographical references
Record ID
BIM-1064511