DocumentCode :
2978953
Title :
Multiobjective H2/H control design for a VSTOL flight model
Author :
Khaniki, M. Salari ; Khosrowjerdi, M.J.
Author_Institution :
Electr. Eng. Dept., Sahand Univ. of Technol., Tabriz, Iran
fYear :
2010
fDate :
11-13 May 2010
Firstpage :
704
Lastpage :
709
Abstract :
In this paper, an application of a multiobjective optimal controller design approach on a multivariable vertical short take-off and landing (VSTOL) aircraft system is presented. To achieve good performance subject to white noises, bounded power disturbances, and to model uncertainties, and to have an acceptable reference tracking, combination of both H2(LQG) and H methods is used. This method uses a time domain game approach for H2/H design. It´s required to solve the corresponding set of coupled algebraic Riccati equations to gain multiobjective controller.
Keywords :
Aerospace control; Aircraft propulsion; Control design; Control systems; Cost function; Design methodology; Hydrogen; Optimal control; Output feedback; Riccati equations; Coupled Algebraic Riccati equations; H2/H control; VSTOL flight control; multiobjective control;
fLanguage :
English
Publisher :
ieee
Conference_Titel :
Electrical Engineering (ICEE), 2010 18th Iranian Conference on
Conference_Location :
Isfahan, Iran
Print_ISBN :
978-1-4244-6760-0
Type :
conf
DOI :
10.1109/IRANIANCEE.2010.5506983
Filename :
5506983
Link To Document :
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