Active nutation damping generally requires a unique element to provide the necessary damping torques, plus a nutation-sensing system to properly monitor and control the active element by closed-loop action. This paper describes and analyzes, a nutation damper for a dual-spin spacecraft which does not require an active element.
Active nutation damping utilizing spacecraft mass properties
Aktive Nutationsdaempfung durch die Masseneigenschaften des Raumfahrzeuges
IEEE Transactions on Aerospace and Electronic Systems ; 9 , 5 ; 688-693
1973
6 Seiten, 7 Bilder, 1 Tabelle, 2 Quellen
Article (Journal)
English
KREISEL , RAUMFAHRZEUG , DAEMPFUNG , REGELKREIS , ZEITKONSTANTE , SPIN , ACHSE
Variable structure controller design for spacecraft nutation damping
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