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...
Saved in:
Published in | Proceedings of 2014 IEEE Chinese Guidance, Navigation and Control Conference pp. 1135 - 1138 |
---|---|
Main Authors | , , , , |
Format | Conference Proceeding |
Language | English |
Published |
IEEE
01.08.2014
|
Subjects | |
Online Access | Get full text |
Cover
Loading…
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 |