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.


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    Title :

    Finite-state analysis of space shuttle contingency guidance requirements


    Contributors:

    Publication date :

    1996-05-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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