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Control of Longitudinal Flight Dynamics of a Flapping-Wing Micro Air Vehicle Using Time-Averaged Model and Differential Flatness Based Controller

Zaeem A. Khan, Sunil K. Agrawal. Control of Longitudinal Flight Dynamics of a Flapping-Wing Micro Air Vehicle Using Time-Averaged Model and Differential Flatness Based Controller. In American Control Conference, ACC 2007, New York, NY, USA, 9-13 July, 2007. pages 5284-5289, IEEE, 2007. [doi]

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