Multicomputer configurations and redundancy management techniques used in various airborne systems were investigated to determine methods to prevent and/or treat generic design flaws. The findings are intended for use in the design of a computer system for use in the space shuttle orbiter.
Prevention of design flaws in multicomputer systems
1975-02-01
Report
Keine Angabe
Englisch
Prevention of design flaws in multicomputer systems
NTRS | 1977
|Some multicomputer configurations for reliability in ATC systems
Tema Archiv | 1974
|Simulation of multicomputer radar systems for ballistic missile defence
Tema Archiv | 1982
|Simulators solve auto design flaws
Tema Archiv | 1992
|