Use of the extended bifurcation analysis method for flight control law design
Author:
Affiliation:
1. Indian Inst. of Technology, Bombay, India
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2002-249
Reference80 articles.
1. Bifurcation Analysis of Nonlinear Aircraft Dynamics
2. Application of bifurcation theory to the high-angle-of-attack dynamics of the F-14
3. Inertia-coupled coordinated roll maneuvers of airplanes
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