Improving Control System Effectiveness for Ducted Fan VTOL UAVs Operating in Crosswinds
Author:
Affiliation:
1. Techsburg
2. AVID LLC
3. Honeywell
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2003-6514
Reference6 articles.
1. 1U.S.Patent6,450,445,September17,2002.
2. 2U.S.Patent4,795,111,January3,1989.
3. Aerodynamic design considerations for a free-flying ducted propeller
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