Hardware development of the wind tunnel based virtual flight system

This paper describes the hardware development for a wind tunnel based virtual flight research project at Low Speed Aeronautics Institution (LSAI). The virtual fight system is outfitted with a rig with spherical rolling joint, dynamics similar aircraft model and flight control system to perform the v...

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Bibliographic Details
Published inProceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference pp. 1135 - 1138
Main Authors Bowen Nie, Linliang Guo, Peng Kong, Min Jiang, Minghong Zhu
Format Conference Proceeding
LanguageEnglish
Published IEEE 01.08.2014
Subjects
Aerodynamics
Aerospace control
Aerospace electronics
Aircraft
Atmospheric modeling
Computers
Mathematical model
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Summary:This paper describes the hardware development for a wind tunnel based virtual flight research project at Low Speed Aeronautics Institution (LSAI). The virtual fight system is outfitted with a rig with spherical rolling joint, dynamics similar aircraft model and flight control system to perform the virtual flight test, This paper provides a detailed summary about the aircraft support rig and test bed, on-board electronic payload, and the various flight testing phases leading to the final virtual flight demonstration in wind tunnel.
ISBN:1479947008
9781479947003
DOI:10.1109/CGNCC.2014.7007362