Optimization procedure to control the coupling of vibration modes in flexible space structures

As spacecraft structural concepts increase in size and flexibility, the vibration frequencies become more closely-spaced. The identification and control of such closely-spaced frequencies present a significant challenge. To validate system identification and control methods prior to actual flight, s...

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Bibliographische Detailangaben

1. Verfasser:	Walsh, Joanne L.
Format:	Tagungsbericht
Sprache:	eng
Schlagworte:	Structural Mechanics
Online-Zugang:	Volltext bestellen
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