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Spacecraft Model Verification Using Swept Sine Data Analysis Hughes Aircraft Company, El Segundo, CA

SAE Technical Papers (1906-current) Available online

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Format:
Conference/Event
Author/Creator:
Fowler, John R., author.
Conference Name:
Aerospace Congress & Exposition (1982-10-25 : Anaheim, California, United States)
Language:
English
Physical Description:
1 online resource
Place of Publication:
Warrendale, PA SAE International 1982
Summary:
Spacecraft sinusoidal vibration test data is analyzed, using overlap processing, to compute transfer functions and to determine frequencies, damping, and modal amplitudes. Results are compared with results obtained from random vibration test data and show excellent agreement. The overlap processing method, therefore, is acceptable for performing system identification computations from typical swept sine vibration test data. Use of alternative reference point for computation of transfer functions is discussed
Notes:
Vendor supplied data
Publisher Number:
821479
Access Restriction:
Restricted for use by site license

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