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)


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

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


    Contributors:

    Publication date :

    1979


    Size :

    41 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





    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 | European Patent Office | 2020

    Free access

    Roll attitude-dependent roll rate limit

    WILSON DOUGLAS L / GRUBB DAVID W / MOREL MARK R | European Patent Office | 2017

    Free access

    Roll attitude-dependent roll rate limit

    WILSON DOUGLAS L / GRUBB DAVID W / MOREL MARK R | European Patent Office | 2020

    Free access