DocumentCode :
1978504
Title :
Deadbeat controller design for high order systems: Application on unmanned aerial vechicle
Author :
Ghazzawi, Yousof M.
Author_Institution :
SABIC Plastic Applic. Dev. Center (SPADC), Saudi Basic Ind. Corp. (SABIC), Riyadh, Saudi Arabia
fYear :
2013
fDate :
19-20 Aug. 2013
Firstpage :
1
Lastpage :
5
Abstract :
This paper describes the design and structural aspects of the advanced proportional integral derivative for nonlinear higher order systems. The design scheme combines deadbeat equation, feedback control, robust control, and the replacement of system zeros with a single gain for simplification purpose. Unlike previous implementations of deadbeat controller, it was possible to apply deadbeat response on a system with a third order zeros without applying any change on the system poles; The design scheme in illustrated on an unmanned aerial vehicle angle of attack. Computer simulation shows that the implemented improvement results on enhanced time domain response and remarkable system robustness to uncertainty.
Keywords :
autonomous aerial vehicles; control system synthesis; feedback; nonlinear control systems; robust control; three-term control; advanced proportional integral derivative control; deadbeat controller design; deadbeat equation; feedback control; nonlinear higher order systems; robust control; simplification purpose; single gain; system robustness; system zeros replacement; time domain response; unmanned aerial vehicle angle-of-attack; Actuators; Conferences; Robustness; Systems engineering and theory; Tuning; Uncertain systems; Nonlinear systems; deadbeat controller; higher order systems; robust control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
System Engineering and Technology (ICSET), 2013 IEEE 3rd International Conference on
Conference_Location :
Shah Alam
Print_ISBN :
978-1-4799-1028-1
Type :
conf
DOI :
10.1109/ICSEngT.2013.6650132
Filename :
6650132
Link To Document :
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