Bifurcation analysis of a model fighter aircraft with control augmentation
- 17 August 1990
- proceedings article
- Published by American Institute of Aeronautics and Astronautics (AIAA)
Abstract
No abstract availableThis publication has 5 references indexed in Scilit:
- 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
- Efficient Numerical Pathfollowing Beyond Critical PointsSIAM Journal on Numerical Analysis, 1987
- Bifurcation Analysis of Nonlinear Aircraft DynamicsJournal of Guidance, Control, and Dynamics, 1982
- Application of high-alpha control system concepts to a variable-sweep fighter airplanePublished by American Institute of Aeronautics and Astronautics (AIAA) ,1980