본 발명은 지면효과를 갖는 쿼드로터에 대한 피드백 선형화기반 슬라이딩 모드 제어 시스템에 관한 발명으로, 폐루프 적분형을 슬라이딩 평면으로 설계하는 슬라이딩 모드 제어에 의해 지면효과 등의 외란에 대해 안정한 쿼드로터의 자세 유지 및 위지 제어 성능을 지닐 수 있는 것을 특징으로 한다.

    The present invention relates to a sliding mode control system based on feedback linearization for a quad-rotor with a ground effect. The sliding mode control system may have posture maintenance and position control performance of a stable quad-rotor against disturbance such as a ground effect by a sliding mode control wherein a closed loop integral type is designed as a sliding plane.


    Access

    Download


    Export, share and cite



    Title :

    Feedback linearization based sliding mode control system for quad-rotor UAV with a Ground effect


    Additional title:

    지면효과를 갖는 쿼드로터에 대한 피드백 선형화기반 슬라이딩 모드 제어 시스템


    Publication date :

    2021-01-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




    Gaussian Process-Based Feedback Linearization Control for Quad-Tiltrotor

    Lee, Dongwoo / Kim, Lamsu / Lee, Jaeho et al. | Springer Verlag | 2022


    Adaptive backstepping sliding mode trajectory tracking control for a quad-rotor

    Gong, X. / Hou, Z. C. / Zhao, C. J. et al. | British Library Online Contents | 2012


    Reduced-Order Observer Based Sliding Mode Control for a Quad-Rotor Helicopter

    Akbar, Reesa / Sumantri, Bambang / Katayama, Hitoshi et al. | British Library Online Contents | 2016