Title :
Modeling and nonlinear control design for a class of hypersonic aircraft
Author :
Zhuang Yifu ; Chen Jie ; Pan Changpeng
Author_Institution :
Navy 91550 Unit, Dalian, China
Abstract :
A six degree-of-freedom nonlinear model of a class of the near space hypersonic aircraft is proposed and modified according to the series of literatures of Winged-Cone offered by America NASA Langly Lab. This model can meet the demand of strong nonlinearity, high coupling, and rapid time variation of hypersonic aircraft control system. Adaptive backstepping method is applied to control design. Both theory analysis and simulation verification show the simpleness and effectiveness of this method.
Keywords :
adaptive control; aircraft control; nonlinear control systems; America NASA Langly Lab; Winged-Cone literature; adaptive backstepping method; nonlinear control design; rapid time variation; space hypersonic aircraft control system; Adaptation models; Aerospace control; Aircraft; Atmospheric modeling; Ear; Military aircraft; NASA; A Six Degree-of-Freedom Nonlinear Model; Adaptive Backstepping; Highly Coupled; Hypersonic Aircraft;
Conference_Titel :
Control Conference (CCC), 2011 30th Chinese
Conference_Location :
Yantai
Print_ISBN :
978-1-4577-0677-6
Electronic_ISBN :
1934-1768
