DocumentCode
3115266
Title
Design of simulation platform for vehicle launching system erecting based on the Vega
Author
Wang, Dandan ; Xu, Bo
Author_Institution
Beijing Inst. of Astronaut. Syst. Eng., China Aerosp. Sci. & Technol. Corp., Beijing, China
fYear
2012
fDate
5-8 Aug. 2012
Firstpage
849
Lastpage
853
Abstract
Horizontal collimation is the development tendency of the vehicle launching system erecting. This paper sets the model of the whole erecting process of vehicle launching system and establishes the simulation platform, which imitates the whole erect process before erecting by 3D Visual Simulation Technique, and realizes the man-machine interaction function at the same time. Then develops the Vega thread in Virtual C++ environment, using Vega API drives vehicle launching model. For this, the platform makes it true that it can describe the calculation accuracy with different navigation mode intuitive and in real time, which provides analysis results for its application and extension, plan making, and precision evaluation.
Keywords
C++ language; application program interfaces; control engineering computing; digital simulation; human computer interaction; inertial navigation; military computing; military vehicles; road vehicles; 3D Visual Simulation Technique; IMU; Vega API; Vega thread; Virtual C++ environment; horizontal collimation; human computer interaction; inertial measurement unit; man-machine interaction function; missile; navigation mode; plan making; precision evaluation; simulation platform design; vehicle launching model; vehicle launching system erection; Analytical models; Data models; Navigation; Solid modeling; Vehicles; Visualization; IMU algorithm simulation; Man-machine interface; Simulation platform; Vega; Vehicle launching system;
fLanguage
English
Publisher
ieee
Conference_Titel
Mechatronics and Automation (ICMA), 2012 International Conference on
Conference_Location
Chengdu
Print_ISBN
978-1-4673-1275-2
Type
conf
DOI
10.1109/ICMA.2012.6283253
Filename
6283253
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