Title :
Research on co-modeling virtual prototype of motion system of flight simulator
Author :
Xiong, Haiguo ; Huang, Qitao ; Ma, Jianming ; Han, Junwei
Author_Institution :
Sch. of Mechatron. Eng., Harbin Inst. of Technol., Harbin, China
Abstract :
Using the traditional mathematical modeling methods to build dynamics model of motion system of flight simulator - - hydraulically driven Stewart platform, there existed defects such as modeling process is relatively complex, simulation can´t provide visual information and so on. To solve the problems, it adopted co-modeling method by combining ADAMS and Matlab/Simulink together, using ADAMS built dynamics model of Stewart platform, using Matlab/Simulink built model of hydraulic servo system and control system, then through seamless interface provided by the software, it established a entire virtual prototype of hydraulically driven Stewart platform. By study and simulation analysis, and then compared with the real Stewart platform through experiments, results showed that the established virtual prototype has high similarity with the real Stewart platform at the performance of dynamics, so it can substitute the general mathematical model to provide theoretical guide and validity in the process of research and development of hydraulically driven Stewart platform. It also proved that the co-modeling method is correct and effective.
Keywords :
aerospace simulation; virtual prototyping; ADAMS simulation; Matlab/Simulink simulation; control system; dynamics model; flight simulator; hydraulic servo system; hydraulically driven Stewart platform; motion system modeling; virtual prototype co-modeling; Aerospace engineering; Aerospace simulation; Analytical models; Automation; Force control; Mathematical model; Mechatronics; Nonlinear dynamical systems; Software prototyping; Virtual prototyping; Stewart platform; co-modeling; dynamics modeling; flight simulator; virtual prototype;
Conference_Titel :
Mechatronics and Automation, 2009. ICMA 2009. International Conference on
Conference_Location :
Changchun
Print_ISBN :
978-1-4244-2692-8
Electronic_ISBN :
978-1-4244-2693-5
DOI :
10.1109/ICMA.2009.5246688