Near-hover control of a helicopter with a hanging load
Author:
Affiliation:
1. Systems Control, Inc., Palo Alto, Calif.
2. Stanford University, Stanford, Calif.
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Aerospace Engineering
Link
http://arc.aiaa.org/doi/pdf/10.2514/3.44521
Reference17 articles.
1. Test Approaches to External Sling Load Instabilities
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