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Spin is a kind of dangerous flight state when aircraft loses control, and it can easily cause flight accident. In order to improve flexibility and anti-spin capability, the limit flight state must be studied. It is the most efficient and safe technology to carry out spin test in vertical wind tunnel. The required test parameter is attitude angles (including pitch, yaw and roll). It briefly introduces...
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,...
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