RISS 학술연구정보서비스

검색
다국어 입력

http://chineseinput.net/에서 pinyin(병음)방식으로 중국어를 변환할 수 있습니다.

변환된 중국어를 복사하여 사용하시면 됩니다.

예시)
  • 中文 을 입력하시려면 zhongwen을 입력하시고 space를누르시면됩니다.
  • 北京 을 입력하시려면 beijing을 입력하시고 space를 누르시면 됩니다.
닫기
    인기검색어 순위 펼치기

    RISS 인기검색어

      검색결과 좁혀 보기

      선택해제

      오늘 본 자료

      • 오늘 본 자료가 없습니다.
      더보기
      • 무료
      • 기관 내 무료
      • 유료
      • KCI등재

        A Parallel-Structure-Based Sliding Mode Control for Trajectory Tracking of a Quadrotor UAV

        Yu Hei-Pei,Wang Minyi,Yang Jiaqianhao,Xiong Jing-Jing 대한전기학회 2023 Journal of Electrical Engineering & Technology Vol.18 No.5

        In this paper, aiming at the problem of incomplete yaw angle working range in a class of sliding mode control for quadrotor unmanned aerial vehicle (UAV), a parallel-structure-based sliding mode control (PSMC) method is proposed. Firstly, the dynamic model of the quadrotor UAV is considered to be composed of fully actuated subsystem and underactuated subsystem. For the fully actuated subsystem, the regular sliding mode manifold is used to design the controller. For the underactuated subsystem, the coordinate transformation of the error is taken into account in the sliding mode manifold. The coefficients of the sliding mode manifold can be obtained by the Hurwitz stability analysis. In addition, the stabilities of two subsystems are demonstrated by Lyapunov theory. Finally, comparative simulation results show that the PSMC not only improve the working range of yaw angle, but also illustrate the effectiveness of the proposed control method.

      연관 검색어 추천

      이 검색어로 많이 본 자료

      활용도 높은 자료

      해외이동버튼