Application of bifurcation theory to the high-angle-of-attack dynamics of the F-14
- 1 January 1994
- journal article
- Published by American Institute of Aeronautics and Astronautics (AIAA) in Journal of Aircraft
- Vol. 31 (1) , 26-34
- https://doi.org/10.2514/3.46451
Abstract
No abstract availableKeywords
This publication has 9 references indexed in Scilit:
- Bifurcation analysis of a model fighter aircraft with control augmentationPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1990
- High-angle-of-attack dynamic behavior of a model high-performance fighter aircraftPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- The various sources of wing rockPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1988
- Nonlinear Oscillations, Dynamical Systems, and Bifurcations of Vector FieldsPublished by Springer Nature ,1983
- Bifurcation Analysis of Nonlinear Aircraft DynamicsJournal of Guidance, Control, and Dynamics, 1982
- Determination of the Spin and Recovery Characteristics of a General Aviation DesignJournal of Aircraft, 1981
- Pseudosteady state analysis of nonlinear aircraft maneuversPublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980
- Elementary Stability and Bifurcation TheoryPublished by Springer Nature ,1980
- Note on a Criterion for Severity of Roll-Induced InstabilityJournal of the Aerospace Sciences, 1959