Title :
Modeling and Simulation of Large Aircraft´s Hybrid Control System
Author :
Li, Zhongjian ; An, Jinwen
Author_Institution :
Coll. of Autom., Northwestern Polytech. Univ., Xi´´an
Abstract :
The research results in the field of modeling and simulation for large aircraft´s hybrid control system is presented. After analyzing the control system structure of the aircraft´s three axes, a method of treating flexible drive of the hybrid mechanism as a hard one is proposed. By means of equivalent dynamic modeling, a complete mathematics model of aircraft´s aileron axis hybrid control system is established. Based on Matlab/Simulink software, an integral develop platform including modeling, design, hardware-in-the-loop simulation and handling qualities assessment is designed. The goal of this platform is low-cost, flexibility, extensibility and modularity. These aim is pursued by eliminating specialized hardware and software solutions and relying on commercial-off-the-shelf components
Keywords :
aerospace simulation; aircraft control; control system CAD; digital simulation; Matlab/Simulink software; aileron axis hybrid control system; aircraft hybrid control system; aircraft modeling; aircraft simulation; commercial-off-the-shelf components; control system structure; equivalent dynamic modeling; flexible drive; hardware-in-the-loop simulation; quality assessment handling; real-time simulation; Aerospace control; Aircraft; Control system analysis; Control system synthesis; Control systems; Hardware; Mathematical model; Mathematics; Quality assessment; Software quality; aircraft hybrid control system; equivalent dynamic model; modeling; real-time simulation;
Conference_Titel :
Intelligent Control and Automation, 2006. WCICA 2006. The Sixth World Congress on
Conference_Location :
Dalian
Print_ISBN :
1-4244-0332-4
DOI :
10.1109/WCICA.2006.1713294
