The Application Research of Aerocraft Simulation System for Speediness prototype and Integrative Modeling

Chao Yun, Xiao-min LI

Abstract


For solve the problem of flight simulation system accurately modeling, speediness and high efficiency implement. It bring forward flight simulation system of aerocraft speediness and integrative modeling method based on Aerosim/RTW. Compare with traditional development method for flight simulation system, the method who based on Aerosim/RTW could implement speediness prototype and integrative process which from digital simulation model establishing to system implement. Lastly the simulation results showed that: this technique based on Aerosim/RTW could achieve speediness prototype and integrative construct for aerocraft dynamic flight simulation system and give birth to remote sensing of flight data flow. The technology have simpleness, conveniency and high efficiency characteristic in the course of constructing for the flight simulation system of aerocraft.

 

DOI : http://dx.doi.org/10.11591/telkomnika.v12i2.3885


Keywords


aerocraft; high efficiency modeling; Aerosim/RTW; speediness and integrative

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Indonesian Journal of Electrical Engineering and Computer Science (IJEECS)
p-ISSN: 2502-4752, e-ISSN: 2502-4760
This journal is published by the Institute of Advanced Engineering and Science (IAES) in collaboration with Intelektual Pustaka Media Utama (IPMU).

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