Computational models for the flight experiment demonstration system (FEDS) code 580 were developed. The FEDS is a modification of the automated orbit determination system which was developed during 1981 and 1982. The purpose of FEDS is to demonstrate, in a simulated spacecraft environment, the feasibility of using microprocessors to perform onboard orbit determination with limited ground support.


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    Title :

    Flight Experiment Demonstration System (FEDS): Mathematical specification


    Contributors:

    Publication date :

    1984-07-01


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English