Feedback Control Logic for Spacecraft Eigenaxis Rotations Under Slew Rate and Control Constraints
Guidance, navigation and control conference ; 1994 ; Scottsdale; AZ
01.01.1994
10 pages
In 3 vols
Aufsatz (Konferenz)
Englisch
AIAA , guidance , navigation , control
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
Feedback Control Logic for Spacecraft Eigenaxis Rotations Under Slew Rate and Control Constraints
Online Contents | 1995
|