Experimental modal analysis for dynamic models of spacecraft

An unconstrained component-mode synthesis technique based on measured modal data for testing solar-array-type structures is presented. A polynomial approximation for the measured modes is introduced to overcome the difficulty involved in synthesizing such a platelike structure; namely, that rotation...

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Veröffentlicht in:Journal of guidance, control, and dynamics control, and dynamics, 1991-05, Vol.14 (3), p.686-688
Hauptverfasser: KOMATSU, KEIJI, SANO, MASAAKI, KAI, TAKASHI, TSUJIHATA, AKIO, MITSUMA, HIDEHIKO
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container_title Journal of guidance, control, and dynamics
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creator KOMATSU, KEIJI
SANO, MASAAKI
KAI, TAKASHI
TSUJIHATA, AKIO
MITSUMA, HIDEHIKO
description An unconstrained component-mode synthesis technique based on measured modal data for testing solar-array-type structures is presented. A polynomial approximation for the measured modes is introduced to overcome the difficulty involved in synthesizing such a platelike structure; namely, that rotational displacements cannot be measured in the usual modal test. The examples that are adduced demonstrate that this method has potential as an alternative for modal tests of a complete structure. (P.D.)
doi_str_mv 10.2514/3.20696
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subjects Aerospace engineering
Dynamic models
Mechanics
Modal analysis
Satellites
title Experimental modal analysis for dynamic models of spacecraft
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