{ "item_title" : "Advanced Aerospace Applications, Volume 1", "item_author" : [" Tom Proulx "], "item_description" : "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.-", "item_img_path" : "https://covers1.booksamillion.com/covers/bam/1/46/142/817/1461428173_b.jpg", "price_data" : { "retail_price" : "219.99", "online_price" : "219.99", "our_price" : "219.99", "club_price" : "219.99", "savings_pct" : "0", "savings_amt" : "0.00", "club_savings_pct" : "0", "club_savings_amt" : "0.00", "discount_pct" : "10", "store_price" : "" } }

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