Title :
Modeling and coupling effects analysis of a High-speed aircraft
Author :
Feng, Dongzhu ; Wang, Xin
Author_Institution :
Sch. of Electron. Eng., Xidian Univ., Xian
Abstract :
The objective of this paper is to accomplish the modeling and coupling effect analysis of a high-speed aircraft. A 2D model of the high-speed aircraft is assumed. The description of the aerodynamic characteristics including forces and moments system models is included in this paper. The analysis and policies of decoupling are put forward based on the data of the high-speed aircraft. Results show that optimization of airframe aerodynamics and control strategy can reduce the effect of coupling. This can be helpful for hypersonic flight control design concepts.
Keywords :
aerodynamics; aircraft control; control system synthesis; force control; optimisation; airframe aerodynamics; forces system; high-speed aircraft; hypersonic flight control; moments system; optimization; Aerodynamics; Aerospace control; Aerospace electronics; Aerospace engineering; Aircraft propulsion; Atmospheric modeling; Drag; Geometry; Mechatronics; Vehicle dynamics; aerodynamics; coupling effects; high-speed aircraft; modeling;
Conference_Titel :
Advanced Intelligent Mechatronics, 2008. AIM 2008. IEEE/ASME International Conference on
Conference_Location :
Xian
Print_ISBN :
978-1-4244-2494-8
Electronic_ISBN :
978-1-4244-2495-5
DOI :
10.1109/AIM.2008.4601822
