Plant equations, autopilot structure and control philosophy are described for the roll control of a vehicle that has destabilizing roll-yaw coupling. Computer-implemented stability analyses and transient responses for two autopilot designs are presented and discussed. (ERA citation 05:004803)


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Roll Control of an Attitude-Controlled Aerodynamic Vehicle Which Has Strong Roll-Yaw Coupling


    Beteiligte:

    Erscheinungsdatum :

    1979


    Format / Umfang :

    41 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





    Efficiency of Aerodynamic Interceptors for Subsonic Missiles Roll Attitude Control

    Mandic, Slobodan D. / Pavic, Milos / Pavkovic, Bojan et al. | AIAA | 2018


    ROLL ATTITUDE-DEPENDENT ROLL RATE LIMIT

    WILSON DOUGLAS L / GRUBB DAVID W / MOREL MARK R | Europäisches Patentamt | 2020

    Freier Zugriff

    Roll attitude-dependent roll rate limit

    WILSON DOUGLAS L / GRUBB DAVID W / MOREL MARK R | Europäisches Patentamt | 2017

    Freier Zugriff

    Roll attitude-dependent roll rate limit

    WILSON DOUGLAS L / GRUBB DAVID W / MOREL MARK R | Europäisches Patentamt | 2020

    Freier Zugriff