This report describes a finite-state analysis of the mode-sequencing requirements for the Contingency Three-Engines-Out Guidance function of the Space Shuttle flight control system.
Finite-state analysis of space shuttle contingency guidance requirements
1996-05-01
Report
No indication
English
Space Shuttle contingency landing operations
NTRS | 1991
|NTIS | 1970
|NTRS | 1970
|Space Shuttle EVA requirements
NTRS | 1973
|