AIAA-2006-6182 Vibration Control of Flexible Spacecraft Under Attitude Maneuver Using Adaptive Controller
AIAA guidance, navigation and control conference ; 2006 ; Keystone, Colo
01.01.2006
20 pages
Paper numbers 2006-6037 to 6807 with gaps held
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Flexible Spacecraft Three Axis Attitude Maneuver by Active Vibration Control
DOAJ | 2009
|British Library Online Contents | 2013
|Networked flexible spacecraft attitude maneuver based on adaptive fuzzy sliding mode control
Online Contents | 2009
|