Title :
Nonlinear modelling and open-loop dynamatics characteristics for one hypersonic aircraft
Author :
Chen, Jie ; Zhao, Hongchao ; Zhuang, Yifu
Author_Institution :
Naval Aeronaut. & Astronaut. Univ., Yantai, China
Abstract :
A six degree-of-freedom nonlinear model of the near space hypersonic aircraft is founded and modified according to the series of literatures of Winged-Cone offered by America NASA Langly Lab. Open-loop dynamatics and stability characteristics show that presented model can meet the demand of strongly nonlinear, highly coupled, rapidly time variation, and be applied to theory study and simulate validation of hypersonic aircraft control system.
Keywords :
aircraft control; vehicle dynamics; America NASA Langly Lab; hypersonic aircraft control system; nonlinear modelling; nonlinear open-loop dynamatics characteristics; space hypersonic aircraft; Adaptation models; Aerospace control; Aircraft; Aircraft navigation; Atmospheric modeling; NASA; Vehicles; A six degree-of-freedom; Hypersonic Aircraft; highly coupled; nonlinear model;
Conference_Titel :
Computer Science and Service System (CSSS), 2011 International Conference on
Conference_Location :
Nanjing
Print_ISBN :
978-1-4244-9762-1
DOI :
10.1109/CSSS.2011.5974109
