Advanced Aerospace Applications, Volume 1: Proceedings of the 29th Imac, a Conference on Structural Dynamics, 2011

High Frequency Optimisation of an Aerospace Structure Through Sensitivity to SEA Parameters.- Converting a Driven Base Vibration Test to a Fixed Base Modal Analysis.- Advanced Operational Modal Analysis Methods for Linear Time Periodic System Identification.- Benefit of Acoustic Particle Velocity Based Reverberant Room Testing of Space Structures.- Ultrasonic Vibration Modal Analysis Technique (UMAT) for Defect Detection.- Acoustic Testing and Response Prediction of the CASSIOPE Spacecraft.- Force Limited Vibration Testing Applied to the JWST FGS OA.- On Force Limited Vibration for Testing Space Hardware.- Calculation of Rigid Body Mass Properties of Flexible Structures.- Simulating Base-shake Environmental Testing.- Geometry-based Updating of 3D Solid Finite Element Models.- A PZT-based Technique for SHM Using the Coherence Function.- The Best Force Design of Pure Modal Test Based Upon a Singular Value Decomposition Approach.- Modal Identification and Model Updating of Pleiades.- Aircraft GVT Advances and Application - Gulfstream G650.- Aircraft Dynamics and Payload Interaction - SOFIA Telescope.- Application of Modal Analysis for Evaluation of the Impact Resistance of Aerospace Sandwich Materials.- An Integrated Procedure for Estimating Modal Parameters During Flight Testing.- Multiple-site Damage Location Using Single-site Training Data.- "Assessment of Nonlinear System Identification Methods Using the.- SmallSat Spacecraft Structure".- Ground Vibration Testing Master Class: Modern Testing and Analysis Concepts Applied to an F-16 Aircraft.- Advanced Shaker Excitation Signals for Aerospace Testing.- System and Method for Compensating Structural Vibrations of an Aircraft Caused by Outside Disturbances.- Operational Modal Analysis on a Modified Helicopter.- Development of New Discrete Wavelet Families for Structural Dynamic Analysis.- Model Updating With Neural Networks and Genetic Optimization.- A Piezoelectric Actuated Stabilization Mount for Payloads Onboard Small UAS.- Extraction of Modal Parameters From Spacecraft Flight Data.- Dynamic Characterization of Satellite Components Through Non-invasive Methods.- An Inertially Referenced Non-contact Sensor for Ground Vibration Tests.- Reliability of Experimental Modal Data Determined on Large Spaceflight Structures.- Operational Modal Analysis of a Spacecraft Vibration Test.-

• Format: Paperback
• Language: English
• ISBN: 1461428173
• ISBN13: 9781461428176
• Release Date: April 2013
• Publisher: Springer
• Length: 368 Pages
• Weight: 1.88 lbs.
• Dimensions: 0.8" x 8.3" x 11.0"