Nonlinear analysis of stability and control for an F-16 configuration
Author:
Affiliation:
1. Kansas, Univ., Lawrence
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.1997-3722
Reference43 articles.
1. ' Mehra, R. K. and Carroll, J. V. "Bifurcation Analysis of Aircraft HighAngle-of-Attack Flight Dynamics,"AIAA Paper 80-1599,Aug. 1980.
2. Application of bifurcation theory to the high-angle-of-attack dynamics of the F-14
3. Analysis and control of bifurcation phenomena in aircraft flight
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