Title :
Nonlinear dynamical model of the aircraft with flight environments
Author :
Lijia, Cao ; Shiyuan, Van ; Yinan, Liu ; Shengxiu, Zhang
Author_Institution :
Lab. of Precise Guidance, Hongqing High-tech Instn., Xi´´an, China
Abstract :
An important research of flight control is the aircraft modeling. In this paper, the influence of flight environment including gravity, wind, and atmosphere is considered when establishing the nonlinear dynamic model of aircraft. The simulation results obtained here indicate that the actual model (with flight environment) is different from that without flight environment. And the influence is great on flight control.
Keywords :
aerospace control; nonlinear dynamical systems; aircraft modeling; flight control; flight environments; nonlinear dynamical model; Aerodynamics; Aircraft; Atmospheric modeling; Integrated circuits; aircraft; dynomic model; flight enviroment;
Conference_Titel :
Computer and Communication Technologies in Agriculture Engineering (CCTAE), 2010 International Conference On
Conference_Location :
Chengdu
Print_ISBN :
978-1-4244-6944-4
DOI :
10.1109/CCTAE.2010.5544803
