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Oct 08, 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 formulations for systems of particles and rigid bodies. Translating and rotating reference frames. Aircraft static stability, aircraft equations of motion, orbital mechanics for the two-body problem, spacecraft rotational dynamics.
Credits: 3 hours
Notes: Open to upperclass and graduate students.
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