A flight vehicle attitude control system design device includes: a gain calculator calculating a proportional gain and a derivative gain from a system natural frequency and a system damping coefficient; a margin calculator calculating a gain margin and a phase margin from the proportional gain and the derivative gain; a grid generator generating a gain-phase margin grid from a relationship between the proportional gain and the derivative gain and a relationship between the gain margin and the phase margin; and a display unit outputting the gain-phase margin grid on a control gain design region having a gain margin as one of a horizontal coordinate axis and a vertical coordinate axis and a phase margin as the other one of the horizontal coordinate axis and the vertical coordinate axis.


    Access

    Download


    Export, share and cite



    Title :

    Flight vehicle attitude control system design method and device


    Contributors:

    Publication date :

    2020-12-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / G01M TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES , Prüfen der statischen oder dynamischen Massenverteilung rotierender Teile von Maschinen oder Konstruktionen / G06F ELECTRIC DIGITAL DATA PROCESSING , Elektrische digitale Datenverarbeitung



    FLIGHT VEHICLE ATTITUDE CONTROL SYSTEM DESIGN METHOD AND DEVICE

    PARK YONG-KYU / SUN BYUNG-CHAN | European Patent Office | 2019

    Free access

    CONTROL METHOD OF ATTITUDE OF FLIGHT VEHICLE AND FLIGHT VEHICLE

    MIWA MASASHI / KURASHIGE HIROTOSHI / TAKEBAYASHI MASAAKI et al. | European Patent Office | 2023

    Free access

    FLIGHT ATTITUDE CONTROL METHOD AND APPARATUS, AND FLIGHT CONTROL SYSTEM

    WU BIN | European Patent Office | 2021

    Free access

    MAP Attitude Control System Design and Flight Performance

    S. F. Andrews / J. R. ODonnell | NTIS | 2002


    MAP Attitude Control System Design and Flight Performance

    Andrews, S. F. / ODonnell, J. R. / Bauer, Frank H. | NTRS | 2002