Title :
Visual Simulation of Flight Attitude Based on MFC and Vega
Author :
Zhonghai, Li ; Shulin, Zhang ; Jianguo, Cui ; Junjie, Gong ; Fen, Yu
Author_Institution :
Coll. of Autom., Shenyang Inst. of Aeronaut. Eng., Shenyang, China
Abstract :
During the study of aircraft key components´ performance, for achieving high efficient and low-cost simulation verification, it´s needed to simulate the flight attitude under different tasks. The visual simulation technology based on flight attitude has been one of the hot topics of current research. In order to design the Aircraft Integrated Health Management System, visual simulation models of horizontal tail were built for multi-attitude flying such as takeoff, landing and large-angle climb, et al. A real-time flight simulation system based on task driving was developed by using of Vega under the MFC framework. The three-dimensional models of key components were driven through Vega API, visual simulation of horizontal tail was achieved during the flight with different attitudes. The conclusion shows, this platform not only provided an intuitionistic interactive interface, but it also was convenient to observe data and performance on simulating, it provides a common visual platform for task-based flight simulation.
Keywords :
aerospace simulation; aircraft maintenance; MFC; Vega API; aircraft integrated health management system; flight attitude; horizontal tail; intuitionistic interactive interface; landing; large-angle climb; multiattitude flying; real-time flight simulation system; simulation verification; takeoff; task-based flight simulation; three-dimensional model; visual simulation model; Atmospheric modeling; Data models; Load modeling; Mathematical model; Numerical models; Object oriented modeling; Visualization; Vega; flight attitude; hardware-in-the-loop simulation; visual simulation;
Conference_Titel :
Information Technology and Applications (IFITA), 2010 International Forum on
Conference_Location :
Kunming
Print_ISBN :
978-1-4244-7621-3
Electronic_ISBN :
978-1-4244-7622-0
DOI :
10.1109/IFITA.2010.69