Title :
Uncertainty modeling for flight control system with wide operation range
Author :
Yan, Yabin ; Zeng, Jianping
Author_Institution :
Dept. of Autom., Xiamen Univ., Xiamen, China
Abstract :
A method of uncertainty modeling is proposed for the flight control system with wide operation range. The model built according to this method contains two parts: one is a polynomial matrix obtained via least square fitting, and the other is the fitting error. The polynomial matrix is related to the parameters and reflects the time-varying characteristic. The fitting error is considered as norm-bounded uncertainties and reflects the uncertain and nonlinear characteristics of the system. And as an example, a model is built for a certain flight control system.
Keywords :
aerospace control; least squares approximations; nonlinear control systems; polynomial matrices; time-varying systems; uncertain systems; fitting error; flight control system; least square fitting; nonlinear characteristic; norm bounded uncertainty; polynomial matrix; time varying characteristic; uncertainty modeling; wide operation range; Aerospace control; Artificial intelligence; Eigenvalues and eigenfunctions; Fitting; Polynomials; Robust control; Uncertainty; 2 norm estimate; flight control system; least square fitting; norm-bounded uncertainty; uncertainty modeling;
Conference_Titel :
Computer Science and Education (ICCSE), 2010 5th International Conference on
Conference_Location :
Hefei
Print_ISBN :
978-1-4244-6002-1
DOI :
10.1109/ICCSE.2010.5593703
