Use of Bifurcation and Continuation Methods for Aircraft Trim and Stability Analysis - A State-of-the-Art
Author:
Affiliation:
1. Indian Institute of Technology, Bombay
2. Indian Institute of Technology, Madras
3. Zeus Numerix Pvt Ltd, IIT Bombay Campus
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2007-1051
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1. The X-31 aircraft: Advances in aircraft agility and performance
2. Numerical Continuation Methods
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4. Inertia-coupled coordinated roll maneuvers of airplanes
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