• DocumentCode
    538824
  • Title

    Research on UAV Degrade Control System under Sensor Fault State

  • Author

    Zhai, Xiaohua ; Liu, Jian´an ; Qian, Zhengzai ; Xin, Gongcai

  • Author_Institution
    First Aeronaut. Inst. of Air Force, Xinyang, China
  • Volume
    2
  • fYear
    2010
  • fDate
    16-17 Dec. 2010
  • Firstpage
    20
  • Lastpage
    23
  • Abstract
    In the low-cost Unmanned Aerial Vehicle (UAV), in order to ensure the security of the system and reduce costs, degrade control system under the sensor fault state is becoming more and more highly regarded. Degrade control adopted less sensor configuration to achieve the desired control functions. In the low-cost prototype UAV research and development process, degrade control not only can reduce system configuration, lower system cost and, more importantly, the degrade control of the system ensures security of the system under the fault state. Attitude control is the most commonly used mode in UAV, and this paper will focus on designing of degrade control of attitude control loop.
  • Keywords
    aircraft control; attitude control; control system synthesis; mobile robots; remotely operated vehicles; sensors; UAV degrade control system; attitude control loop; sensor fault state; unmanned aerial vehicle; Aircraft; Attitude control; Control systems; Damping; Turning; Unmanned aerial vehicles; Attitude Control; Degrade Control; Fault; Sensor;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Intelligent Systems (GCIS), 2010 Second WRI Global Congress on
  • Conference_Location
    Wuhan
  • Print_ISBN
    978-1-4244-9247-3
  • Type

    conf

  • DOI
    10.1109/GCIS.2010.189
  • Filename
    5708669