MAE 3405
FLIGHT DYNAMICS.
University of Texas at Arlington · UGRD · Fall 2026
1 section
Catalog description
Derivation of equation of motion (EOM) of a flight vehicle. Trimmed flight condition analysis based on the nonlinear EOM. Linearization of EOM for a given trimmed flight condition. State-space and transfer-function representations of the linear EOM. Aircraft stability and dynamic performance analysis based on the linear EOM. Prerequisite: Must be in the professional ME or AE program and C or better in each of the following, MAE 3306 and MATH 3330 ; or student group.
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Availability not recently verifiedClass #texas_arlington-4199Fall 2026UGRD4 credits
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