Intelligent method based coordinated integrated flight control of a tailless STOVL

Author

Fan, Yong ; Zhu, J.-H. ; Meng, X.-Y. ; Liu, Kai ; Yang, X.-L.

Author_Institution

Dept. of Comput. Sci. & Technol., Tsinghua Univ., Beijing, China

fYear

2010

Firstpage

85

Lastpage

90

Abstract

The ability of Vertical and/or Short Take-Off and Landing is the objective of advanced fighter and shipboard fighter. In this paper we proposed a prototype of tailless configured STOVL aerial vehicle. Based on which, the mathematical model was studied by mechanical analysis and CFD (Computing Fluid Dynamics) computation. Besides, an intelligent adaptive based control law was proposed and the optimization approach is employed to solve the constrained control allocation problem. The results show good closed loop performance and validate the intelligent optimization approach of constrained control allocation for flight control.

Keywords

adaptive control; aircraft control; closed loop systems; computational fluid dynamics; intelligent control; optimisation; space vehicles; CFD; advanced fighter; closed loop performance; computing fluid dynamics computation; constrained control allocation problem; coordinated integrated flight control; intelligent adaptive based control law; intelligent method; intelligent optimization approach; mathematical model; mechanical analysis; shipboard fighter; tailless STOVL; tailless configured STOVL aerial vehicle; vertical and/or short take-off and landing; Aerospace control; Computational fluid dynamics; Computer languages; Moment methods; Optimization; Resource management; Vehicles; STOVL; dynamic modeling; flight control; tailless configured aerial vehicle;

fLanguage

English

Publisher

ieee

Conference_Titel

Intelligent Control and Automation (WCICA), 2010 8th World Congress on

Conference_Location

Jinan

Print_ISBN

978-1-4244-6712-9

Type

conf

DOI

10.1109/WCICA.2010.5553863

Filename

5553863