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AER E 355: Aircraft Flight Dynamics and Control

(3-0) Cr. 3. F.S.

Prereq: AER E 261, MATH 267, E M 345
Aircraft rigid body equations of motion, linearization, and modal analysis. Longitudinal and lateral-directional static and dynamic stability analysis. Flight handling characteristics analysis. Longitudinal and lateral-directional open loop response to aircraft control inputs. Aircraft flight handling qualities.