Three examples show problems involved in selection of possible trajectories; objective is to select path which will best accomplish mission within constraints imposed by payload weight, scientific experiment requirements, and systems which control flight path; Mars orbiter mission shows these interactions; 2-way Doppler measurements taken on flight of Mariner 2 to Venus can give independent determination of astronomical unit, mass of Venus, and location of primary ground tracking station; 3-dimensional model used at Jet Propulsion Laboratory demonstrates how tracking "geometry" of different stations contributes to determination of target errors.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Applications of celestial mechanics to spacecraft flight


    Weitere Titelangaben:

    NASA -- University Conference Science Technology Space Exploration -- Proc


    Beteiligte:
    Hamilton, T.W. (Autor:in)

    Kongress:

    Proceedings of the University Conference on National Aeronautics and Space Administration University Conference on Science and Technology of Space Exploration ; 1962 Orbits and trajectories



    Erscheinungsdatum :

    1962


    Format / Umfang :

    8 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Celestial Mechanics

    Stark, John P. W. / Swinerd, Graham G. / Fortescue, Peter W. | Wiley | 2011


    Celestial mechanics

    Anderson, J. D. / Efron, L. / Wong, S. K. | NTRS | 1969


    Celestial mechanics experiment

    Anderson, J. D. / Efron, L. / Pease, G. E. et al. | NTRS | 1967


    Astrodynamics and celestial mechanics

    Szebehely, Victor G. | TIBKAT | 1971


    Celestial mechanics and Spaceflight

    Uffrecht, U. / European Space Agency | British Library Conference Proceedings | 2002