Parafoil steady turn response to control input
Author:
Affiliation:
1. Vertigo, Inc., Lake Elsinore, CA
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1993-1241
Reference4 articles.
1. Goodrick, T. F. "Scale Effects on Performance of Ram Air Wingsw,AIAA 84-0783, 1984 0 0 05 0 1 0 15 0 2 C
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