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Adaptive model reference control of highly maneuverable high performance aircraft

Creator:

Collins, David C. (David Charles), 1969-

Abstract:

This thesis presents an adaptive model reference controller for a highly maneuverable high performance aircraft, in particular, a modified F18. An adaptive controller is developed to maneuver an aircraft at a high angle of attack. Thus, the aircraft is required to fly over a highly nonlinear flight regime. The adaptive...

Resource Type:

Masters Thesis

Full Text:

Adaptive model reference control of highly maneuverable