Various representations of the aerodynamic contribution to the aircraft's equation of motion are shown to be compatible within the common assumption of their Frechet differentiability. Three forms of invalidating Frechet differentiality are identified, and the mathematical model is amended to accommodate their occurrence. Some of the ways in which chaotic behavior may emerge are discussed, first at the level of the aerodynamic contribution to the equation of motion, and then at the level of the equations of motion themselves.
Modeling Aerodynamic Discontinuities and the Onset of Chaos in Flight Dynamical Systems
1986
50 pages
Report
No indication
English
Modeling aerodynamic discontinuities and onset of chaos in flight dynamical systems
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