Application of dynamical systems theory to nonlinear aircraft dynamics

Application of dynamical systems theory to nonlinear aircraft dynamics

<p>A continuation method has been used to determine the steady states of three nonlinear aircraft models: a general aviation aircraft with a canard configuration, a generic jet fighter, and the F-14. The continuation method calculated the steady states of the aircraft as functions of the contr...

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Bibliographic Details
Main Author: Jahnke, Craig C.
Format: Others
Published: 1990
Online Access:https://thesis.library.caltech.edu/1708/1/Jahnke_cc_1990.pdf
Jahnke, Craig C. (1990) Application of dynamical systems theory to nonlinear aircraft dynamics. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/9KZS-XC46. https://resolver.caltech.edu/CaltechETD:etd-05092007-134504 <https://resolver.caltech.edu/CaltechETD:etd-05092007-134504>

Internet

https://thesis.library.caltech.edu/1708/1/Jahnke_cc_1990.pdf
Jahnke, Craig C. (1990) Application of dynamical systems theory to nonlinear aircraft dynamics. Dissertation (Ph.D.), California Institute of Technology. doi:10.7907/9KZS-XC46. https://resolver.caltech.edu/CaltechETD:etd-05092007-134504 <https://resolver.caltech.edu/CaltechETD:etd-05092007-134504>

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