• DocumentCode
    539628
  • Title

    Control System Design and Simulation of an Aerial Three-Axis ISP System Based on SimMechanics

  • Author

    Jianping, Li ; Xiangyang, Zhou ; Quanqi, Mu ; Du Lei

  • Author_Institution
    Sch. of Instrum. Sci. & Opto-Electron. Eng., Beijing Univ. of Aeronaut. & Astronaut., Beijing, China
  • Volume
    1
  • fYear
    2011
  • fDate
    6-7 Jan. 2011
  • Firstpage
    778
  • Lastpage
    781
  • Abstract
    The main purpose of this paper is to investigate the control method for a three-axis ISP. Firstly, a simplified geometry model was built by Solid works. Then, a Simulink model composed of bodies, joints, constraints, and force elements of ISP was obtained from the 3D model via SimMechanic toolbox. On the basis of the Simulink model, the classical PID controllers and three closed servo loops were designed and applied to the ISP system under the friction disturbance being taken into account. The simulation results show that compared to the roll and pitch gimbals, the dynamic performance of the yaw gimbal is severely affected by the friction and whose proportion in position loop needs to be adjusted if a better dynamic performance is got.
  • Keywords
    aerospace instrumentation; closed loop systems; control engineering computing; inertial systems; servomechanisms; solid modelling; three-term control; PID controllers; SimMechanics; Simulink model; Solidworks; aerial three axis ISP system; closed servo loops; control system design; geometry model; pitch gimbals; roll gimbals; yaw gimbal; Friction; Image sensors; Interference; Remote sensing; Servomotors; Solid modeling; PID; Servo Control; SimMechanic; Three-Axis ISP;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Measuring Technology and Mechatronics Automation (ICMTMA), 2011 Third International Conference on
  • Conference_Location
    Shangshai
  • Print_ISBN
    978-1-4244-9010-3
  • Type

    conf

  • DOI
    10.1109/ICMTMA.2011.196
  • Filename
    5720899