A unique ground control system was designed and implemented to support and meet the stringent mission requirements of the SAS-1. The important features of the system are described with emphasis on the software used to control the orientation of the spacecraft. A summary of the system's operation during the SAS-1 mission is given along with a discussion of the performance of the software subsystems relative to the mission requirements.
SAS Attitude Support System
1972-01-01
Aufsatz (Konferenz)
Keine Angabe
Englisch
RAE-A attitude determination ground support system
AIAA | 1970
|RAE-A attitude determination ground support system
NTRS | 1970
|