The development and use of an interactive environment to perform control system design and analysis of the proposed Crew Exploration Vehicle Launch Abort System is described. The environment, built using a commercial dynamic systems design package, includes use of an open-source configuration control software tool and a collaborative wiki to coordinate between the simulation developers, control law developers and users. A method for switching between multiple candidate control laws and vehicle configurations is described. Aerodynamic models, especially in a development program, change rapidly, so a means for automating the implementation of new aerodynamic models is described.


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    Title :

    Simulation Environment for Orion Launch Abort System Control Design Studies


    Contributors:

    Conference:

    AIAA Modeling and Simulation Technologies Conference ; 2007 ; Hilton Head, SC, United States


    Publication date :

    2007-08-20


    Type of media :

    Conference paper


    Type of material :

    No indication


    Language :

    English




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