DocumentCode
2056361
Title
Notice of Violation of IEEE Publication Principles
Optimal control synthesis for UAV
Author
Hussain, Syed Asad ; Kadri, Muhammad Bilal
Author_Institution
Dept. of Electr. Power Eng., Nat. Univ. of Sci. & Technol. (NUST), Islamabad, Pakistan
fYear
2013
fDate
25-26 Sept. 2013
Firstpage
1
Lastpage
6
Abstract
Notice of Violation of IEEE Publication Principles
"Optimal Control Synthesis for UAV"
by Syed Asad Hussain and Muhammad Bilal Kadri
in the 2013 Proceedings of the International Conference on Computer,Control & Communication (IC4)
After careful and considered review of the content and authorship of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE???s Publication Principles.
This paper contains significant portions of original text from the paper cited below. The original text was copied without attribution (including appropriate references to the original author(s) and/or paper title) and without permission.
"H2 and H~ Robust Autopilot Synthesis for Longitudinal Flight of a Special Unmanned Aerial Vehicle: A Comparative Study"
by F. Santoso, M. Liu, and G. Egan,
in IET Control Theory and Applications, Vol 2, No 7, 2008.
This paper present a method for the solution of the fundamental output feedback H2 (linear quadratic Gaussian or LQG) and H∞ control problem (with frequency weights for performance enhancement and loop shaping) for unmanned aerial vehicle (UAV), P-15035 aircraft that has elevon control. Aim is to put together a state-space elucidation of optimal controller, under less restrictive condition of relationships. H2 (Linear quadratic Gaussian or LQG) and H∞ controllers are realized to overcome uncertainties of real environment. Simulation results illustrate that robust performance is realized with reasonably good stability performance. Developments / progress through this research can the incorporated in intended autopilots.
"Optimal Control Synthesis for UAV"
by Syed Asad Hussain and Muhammad Bilal Kadri
in the 2013 Proceedings of the International Conference on Computer,Control & Communication (IC4)
After careful and considered review of the content and authorship of this paper by a duly constituted expert committee, this paper has been found to be in violation of IEEE???s Publication Principles.
This paper contains significant portions of original text from the paper cited below. The original text was copied without attribution (including appropriate references to the original author(s) and/or paper title) and without permission.
"H2 and H~ Robust Autopilot Synthesis for Longitudinal Flight of a Special Unmanned Aerial Vehicle: A Comparative Study"
by F. Santoso, M. Liu, and G. Egan,
in IET Control Theory and Applications, Vol 2, No 7, 2008.
This paper present a method for the solution of the fundamental output feedback H2 (linear quadratic Gaussian or LQG) and H∞ control problem (with frequency weights for performance enhancement and loop shaping) for unmanned aerial vehicle (UAV), P-15035 aircraft that has elevon control. Aim is to put together a state-space elucidation of optimal controller, under less restrictive condition of relationships. H2 (Linear quadratic Gaussian or LQG) and H∞ controllers are realized to overcome uncertainties of real environment. Simulation results illustrate that robust performance is realized with reasonably good stability performance. Developments / progress through this research can the incorporated in intended autopilots.
Keywords
H∞ control; H2 control; aircraft control; autonomous aerial vehicles; control system synthesis; feedback; linear quadratic Gaussian control; mobile robots; performance index; position control; realisation theory; robust control; state-space methods; uncertain systems; H∞ control problem; H∞ controller realization; LQG; P-15035 aircraft; UAV; altitude control; autopilot; elevon control; environment uncertainties; frequency weight; linear quadratic Gaussian control problem; loop shaping; optimal control synthesis; output feedback H2 control problem; performance enhancement; robust performance; stability performance; state-space elucidation; unmanned aerial vehicle; Aerodynamics; Aerospace control; Aircraft; Output feedback; Robustness; Transfer functions; Vehicle dynamics;
fLanguage
English
Publisher
ieee
Conference_Titel
Computer,Control & Communication (IC4), 2013 3rd International Conference on
Conference_Location
Karachi
Print_ISBN
978-1-4673-6011-1
Type
conf
DOI
10.1109/IC4.2013.6653743
Filename
6653743
Link To Document