Study program written in FORTRAN 4 developes an oribital rendezvous guidance scheme for large, constant thrust launch vehicles. It concentrates on /1/ an investigation of the direct extension of the present Saturn Iterative Guidance Mode /IGM/ scheme and /2/ a scheme formulated in a reference frame moving with the target satellite.


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    Title :

    Earth orbit rendezvous evaluation program


    Contributors:

    Publication date :

    1967-11-01


    Type of media :

    Miscellaneous


    Type of material :

    No indication


    Language :

    English




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