Bifurcation Analysis of Rotorcraft Dynamics with an Underslung Load
Author:
Affiliation:
1. University of Bristol
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2004-4947
Reference22 articles.
1. 3MacMillen, F., Continuation and Bifurcation Analysis of Flight Dynamics for Combat Aircraft: An Assessment for the Aircraft Industry, MSc thesis, Centre for Nonlinear Dynamics and its Applications,University College, London,Sept. 1996.
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