Input Shaping for Helicopter Slung Load Swing Reduction
Author:
Affiliation:
1. Aalborg University
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2008-6964
Reference22 articles.
1. 10 20 30 40 50 60 70 80 -2 -1 0 1 2 Steps without shaper
2. 10 20 30 40 50 60 70 80 -4
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