DocumentCode
3521785
Title
Research on Aeroservo-Thermoelasticity for a Supersonic Aircraft
Author
Tang Hong ; Chen Guoguang ; Hua Cheng
Author_Institution
Sch. of Mechatron. Eng., North Univ. of China, Taiyuan, China
fYear
2011
fDate
28-29 May 2011
Firstpage
1
Lastpage
4
Abstract
The vibration mode frequency and the coupling of supersonic aircraft could be changed by aerodynamic heat. The problem of aero-thermo-elasticity (ATE) was solved by coupling system of motion stress equations and heat flow conservation equations. The aero-servo-thermo-elasticity (ASTE) is a coupling system included ATE and control system. In the ASTE, control system is adopted to Proportional-Integral-Differential (PID) method.
Keywords
aerodynamics; aircraft; aircraft control; heat transfer; thermoelasticity; three-term control; vibrations; aerodynamic heat; aeroservothermoelasticity; control system; heat flow conservation equation; motion stress equation; proportional integral differential method; supersonic aircraft; vibration mode frequency; Aerodynamics; Aerospace control; Aircraft; Aircraft propulsion; Control systems; Couplings; Equations;
fLanguage
English
Publisher
ieee
Conference_Titel
Intelligent Systems and Applications (ISA), 2011 3rd International Workshop on
Conference_Location
Wuhan
Print_ISBN
978-1-4244-9855-0
Electronic_ISBN
978-1-4244-9857-4
Type
conf
DOI
10.1109/ISA.2011.5873414
Filename
5873414
Link To Document