NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Back to Results
Lumped Parameter Modeling for Rapid Vibration Response Prototyping and Test Correlation for Electronic UnitsPresent preliminary work using lumped parameter models to approximate dynamic response of electronic units to random vibration; Derive a general N-DOF model for application to electronic units; Illustrate parametric influence of model parameters; Implication of coupled dynamics for unit/board design; Demonstrate use of model to infer printed wiring board (PWB) dynamics from external chassis test measurement.
Document ID
20150007452
Acquisition Source
Jet Propulsion Laboratory
Document Type
Presentation
External Source(s)
Authors
Van Dyke, Michael B.
(Jet Propulsion Lab., California Inst. of Tech. Pasadena, CA, United States)
Date Acquired
May 6, 2015
Publication Date
June 4, 2013
Subject Category
Structural Mechanics
Meeting Information
Meeting: Spacecraft and Launch Vehicle Dynamic Environments Workshop
Location: El Segundo, CA
Country: United States
Start Date: June 4, 2013
End Date: June 6, 2013
Sponsors: Aerospace Corp.
Distribution Limits
Public
Copyright
Other
Keywords
random vibration
electronic units
test correlation
lumped parameter modeling

Available Downloads

There are no available downloads for this record.
No Preview Available