Attitude Control of a Small UAV Using a Flow Sensor System
Author:
Affiliation:
1. Faculty of Mechanical Engineering, Kanazawa University
2. Department of Aerospace Engineering, Osaka Prefecture University
Publisher
Japan Society of Mechanical Engineers
Link
https://www.jstage.jst.go.jp/article/jsdd/5/1/5_1_1/_pdf
Reference18 articles.
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2. (2) Gad-el-Hak, Mohamed, Flow Control: The Future, Journal of Aircraft, Vol. 38, No. 3(2001), pp. 402-418.
3. (3) Gerontakos, P., and Lee, T., Dynamic Stall Flow Control via a Trailing-Edge Flap, AIAA Journal, Vol.44, No. 3(2006), pp. 469-480.
4. (4) Gerontakos, P., and Lee, T., Active Trailing-Edge Flap Control of Oscillating-Wing Tip Vortex, AIAA Journal, Vol. 44, No. 11(2006), pp. 2746-2754.
5. (5) Feszty, D., Gillies, E. A., and Vezza, M., Alleviation of Airfoil Dynamic Stall Moments via Trailing-Edge-Flap Flow Control, AIAA Journal, Vol. 42, No. 1(2004), pp.17-25.
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