The Gamma Guidance Algorithm which controls the inertial upper stage is described. The results of an independent assessment of the algorithm's performance in satisfying the NASA missions' targeting objectives are presented. The results of a launch window analysis for a Galileo mission, and suggested improvements are included.
IUS Guidance Algorithm gamma Guide Assessment
1980
54 pages
Report
Keine Angabe
Englisch
IUS guidance algorithm gamma guide assessment
NTRS | 1980
|Conceptual Spacecraft-Guidance Algorithm
NTRS | 1988
|