Title :
Integrated modeling and simulation for CAV aerodynamic and control
Author :
Feng, Zhigao ; Xiao, Jin ; Lin, Ping
Author_Institution :
School of Astronautics Beihang University, Beijing, 100191, China
Abstract :
An aerodynamic and control integrated modeling and simulation approach is developed based on MATLAB in this paper. The parametric configuration generation method and aerodynamic engineering method is used to rapidly calculate aerodynamic forces. The LQR controller is designed to track attitude commands. With combination of aerodynamic calculation and control system on the MATLAB platform, the real-time simulation is conducted effectively and the results demonstrate the integrated approach.
Keywords :
CAV; aerodynamic calculation; control design; real-time simulation;
Conference_Titel :
Modelling, Identification & Control (ICMIC), 2012 Proceedings of International Conference on
Conference_Location :
Wuhan, Hubei, China
Print_ISBN :
978-1-4673-1524-1
