The development of a candidate autonomous onboard Mars approach navigation scheme capable of supporting aerocapture into Mars orbit is discussed. An aerocapture guidance and navigation system which can run independently of the preaerocapture navigation was used to define a preliminary set of accuracy requirements at entry interface. These requirements are used to evaluate the proposed preaerocapture navigation scheme. This scheme uses optical sightings on Deimos with a star tracker and an inertial measurement unit for instrumentation as a source for navigation nformation. Preliminary results suggest that the approach will adequately support aerocaputre into Mars orbit.


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    Titel :

    An onboard navigation system which fulfills Mars aerocapture guidance requirements


    Beteiligte:

    Erscheinungsdatum :

    1989-01-01


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Keine Angabe


    Sprache :

    Englisch


    Schlagwörter :


    An onboard navigation system which fulfills Mars aerocapture guidance requirements

    BRAND, TIMOTHY / FUHRY, DOUGLAS / SHEPPERD, STANLEY | AIAA | 1989


    A design study of onboard navigation and guidance during aerocapture at Mars

    Fuhry, Douglas Paul | DSpace@MIT | 1988

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