Title :
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
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;
Conference_Titel :
Intelligent Control and Automation (WCICA), 2010 8th World Congress on
Conference_Location :
Jinan
Print_ISBN :
978-1-4244-6712-9
DOI :
10.1109/WCICA.2010.5553863
