A conventional virtual flight test generally refers to a 3-DOF dynamic flight test in a wind tunnel. In the wind tunnel test, the model aircraft is connected to the strut through a 3-DOF rotation mechanism and installed in the wind tunnel test section so that the model displacement is constrained but has 3 degrees of angular motion freedom. Open-loop and closed-loop control of the aircraft model is achieved by directly driving the rudder surface or by using commands from the flight control system.

DOI Link: 
10.21227/yc97-ys48
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[1] Shang Tai, Lixin Wang, Yanling Wang, Shiguang Lu, Chen Bu, "A 3/4-DOF Wind Tunnel Virtual Flight Test", IEEE Dataport, 2022. [Online]. Available: http://dx.doi.org/10.21227/yc97-ys48. Accessed: Dec. 02, 2024.
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doi = {10.21227/yc97-ys48},
url = {http://dx.doi.org/10.21227/yc97-ys48},
author = {Shang Tai; Lixin Wang; Yanling Wang; Shiguang Lu; Chen Bu },
publisher = {IEEE Dataport},
title = {A 3/4-DOF Wind Tunnel Virtual Flight Test},
year = {2022} }
TY - DATA
T1 - A 3/4-DOF Wind Tunnel Virtual Flight Test
AU - Shang Tai; Lixin Wang; Yanling Wang; Shiguang Lu; Chen Bu
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PB - IEEE Dataport
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Shang Tai, Lixin Wang, Yanling Wang, Shiguang Lu, Chen Bu. (2022). A 3/4-DOF Wind Tunnel Virtual Flight Test. IEEE Dataport. http://dx.doi.org/10.21227/yc97-ys48
Shang Tai, Lixin Wang, Yanling Wang, Shiguang Lu, Chen Bu, 2022. A 3/4-DOF Wind Tunnel Virtual Flight Test. Available at: http://dx.doi.org/10.21227/yc97-ys48.
Shang Tai, Lixin Wang, Yanling Wang, Shiguang Lu, Chen Bu. (2022). "A 3/4-DOF Wind Tunnel Virtual Flight Test." Web.
1. Shang Tai, Lixin Wang, Yanling Wang, Shiguang Lu, Chen Bu. A 3/4-DOF Wind Tunnel Virtual Flight Test [Internet]. IEEE Dataport; 2022. Available from : http://dx.doi.org/10.21227/yc97-ys48
Shang Tai, Lixin Wang, Yanling Wang, Shiguang Lu, Chen Bu. "A 3/4-DOF Wind Tunnel Virtual Flight Test." doi: 10.21227/yc97-ys48