Title :
Elastic disturbance modeling and analysis for hypersonic vehicle
Author :
Han Huilian ; Liu Xiujuan
Author_Institution :
Nat. Key Lab. of Sci. & Technol. on Aerosp. Intell. Control, Beijing, China
Abstract :
To achieve precise control of hypersonic vehicle, the paper analyzed the effects of flexible vibration on the hypersonic vehicle flight control system, a non-linear physics-based dynamic model including the impacts of structure, aerodynamic, thrust system coupling and elastic impact for an air-breathing hypersonic vehicle was developed. One of the main disturbance-coupling between elastic mode and rigid state was modeled and analyzed. A disturbance observer was designed and simulated. Simulations results are provided to validate the proposed approach.
Keywords :
aerodynamics; aircraft control; elasticity; nonlinear control systems; observers; vibrations; aerodynamics; air-breathing hypersonic vehicle; disturbance observer; elastic disturbance analysis; elastic disturbance modeling; elastic impact; flexible vibration; hypersonic vehicle control; hypersonic vehicle flight control system; nonlinear physics-based dynamic model; thrust system coupling; Aerodynamics; Analytical models; Atmospheric modeling; Couplings; Observers; Vehicle dynamics; Vehicles; Disturbance Estimation; Disturbance Observer; Flexible Vibration; Hypersonic Vehicle; Nonlinear Dynamic Model;
Conference_Titel :
Mechatronic Sciences, Electric Engineering and Computer (MEC), Proceedings 2013 International Conference on
Conference_Location :
Shengyang
Print_ISBN :
978-1-4799-2564-3
DOI :
10.1109/MEC.2013.6885075
