Flight control requirements of reusable launch vehicles are reviewed and compared to those of aircraft, current launch vehicles, and spacecraft. Areas are identified in which more work on the flight control system will improve mission performance. Current work in three areas is briefly reviewed - the use of man in the control loop, the development of systems which can accommodate large changes in the flight conditions, and use of the flight control system to reduce wind-induced loading.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Control Systems for Reusable Launch Vehicles


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Space Technology Conference ; 1967



    Erscheinungsdatum :

    1967-02-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch




    Control systems for reusable launch vehicles.

    Blair, J. C. / Redus, J. R. | NTRS | 1967


    Reusable launch vehicles

    Osmun, W.G. | Engineering Index Backfile | 1964


    Reusable launch vehicles

    DrDr Ruppe, H.O. | Elsevier | 1985



    Future reusable launch vehicles

    American Institute of Aeronautics and Astronautics / International Astronautical Federation | British Library Conference Proceedings | 2002