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Tuesday, 1:45 PM - 3:45 PM

Technical

Presentations

Note: Presentations may start a few minutes before the time listed in the schedule.

Participant RoleDetailsStart TimeMinutesAction
SubmissionFree Vibration Analysis of Rotating Rayleigh Cantilever Beam Using P-Type Finite Element Method01:45 PM30View
SubmissionExperimental Validation of Cubesat On-Orbit Vibration Data via Ground Tests02:15 PM30View
SubmissionNonlinear Model Predictive Control of Urban Air Mobility Aircraft for Vibration Suppression and Trajectory Tracking02:45 PM30View
SubmissionResonance Prediction for an Assembly of Two Parts Having Similar Frequencies03:15 PM30View
Total:120 Minute(s)

02-01-02: Dynamic Loads, Response, Vibration and Alleviation of Aerospace Structures - II