Most UAV configurations are conventional, aerodynamically driven shapes, with conventional stability AND control characteristics. However, the requirements of Combat UAVs (UCAVs) drive to radical configurations with unusual stability AND control challenges: Finless - Rudderless - High wing sweep - Unusual wing shapes - Blended wing-bodies - No forebody. Stability AND control issues must be addressed early in the UCAV design cycle.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Aeroacoustic Assessment of Low-Observable UCAV Configurations

    Rossignol, Karl-Stephane / Proskurov, Stanislav / Lummer, Markus et al. | Deutsches Zentrum für Luft- und Raumfahrt (DLR) | 2020

    Freier Zugriff

    UCAV

    Online Contents | 1998


    MEGLADON - Interception UCAV

    Dagan, A. / Shtayer, D. / Ozeri, E. et al. | British Library Conference Proceedings | 2001


    UCAV Integration

    Campbell, N. / Royal Aeronautical Society | British Library Conference Proceedings | 2007


    New projects: UCAV

    Online Contents | 1997