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Nov 24, 2024
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AE 5400 - Aerospace Vehicle Dynamics Three-dimensional kinematics and dynamics with a focus on aerospace vehicles. Newton/Euler and Lagrangian and Kane’s formulations for systems of particles and rigid bodies. Translating and rotating reference frames. Aircraft 6-DOF equations of motion, orbital mechanics for the two-body problem.
Prerequisites & Corequisites: Prerequisites: ME 2580 and ME 3600, with a grade of “B” or better in all prerequisites.
Credits: 3 hours
Notes: Open to upper level and graduate students.
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