On Nonlinear Dynamics and an Optimal Control Design to a Longitudinal Flight
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2008-01-01
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Asme-amer Soc Mechanical Eng
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In this work, we analyzed a bifurcational behavior of a longitudinal flight nonlinear dynamics, taking as an example the F-8 aircraft Crusader. We deal with an analysis of high angles of attack in order to stabilize the oscillations; those were close to the critical angle of the aircraft, in the flight conditions, established. We proposed a linear optimal control design applied to the considered nonlinear aircraft model below angle of stall, taking into account regions of Hopf and saddled noddle bifurcations.
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Journal of Computational and Nonlinear Dynamics. New York: Asme-amer Soc Mechanical Eng, v. 3, n. 1, p. 6, 2008.