A methodology for autonomous spacecraft design blends autonomy requirements with traditional mission requirements and assesses the impact of autonomy upon the total system resources available to support fault-tolerance and automation. A baseline functional design can be examined for autonomy implementation impacts, and the costs, risk, and benefits of various options can be assessed. The result of the process is a baseline design that includes autonomous control functions.
Autonomous spacecraft design methodology
IECEC ''84: Advanced energy systems - Their role in our future ; 1984 ; San Francisco, CA
01.01.1984
Aufsatz (Konferenz)
Keine Angabe
Englisch
Fault tolerant design and autonomous spacecraft
AIAA | 1981
|NTRS | 1982
|Tema Archiv | 1986
|Command and telemetry in autonomous spacecraft design
NTRS | 1984
|