Application of Piezoceramics to Vibration Suppression of a Spacecraft Flexible Appendage
Conference, AIAA guidance navigation and control conference ; 1996 ; San Diego; CA
01.01.1996
ALL
Nos 96-3690 to 96-3929 with gaps held only; See also 6369.400F for paper nos 96-3690 to 96-3962 with gaps held on fiche
Aufsatz (Konferenz)
Englisch
AIAA , guidance , navigation
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Specifying spacecraft flexible appendage rigidity
AIAA | 1977
|Specifications of Spacecraft Flexible Appendage Rigidity
AIAA | 1978
|Vibration suppression of flexible spacecraft during attitude control
Online Contents | 2001
|