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Published on Aug 6, 2012
This is a video clip of the Coanda disk aircraft trial with the airframe mounted on a vertical torsion balance but with no dynamic torque cancellation and vertical axis attitude (steering) mechanism fitted. A following clip shows the operation of the torque cancellation and vertical axis attitude control (steering) mechanism which is called the Director. This clip was part of a presentation to an international audience of engineers and scientists at the 18th International Conference on Unmanned Air vehicles held at Bristol University in 2001. Read the full paper at www.coanda.co.uk