• DocumentCode
    438923
  • Title

    Integrated guidance/autopilot scheme for anti-vessel missiles based on three channels independence design idea

  • Author

    Zhao, Guorong ; Xu, Qingjiu ; Yu, Jinyong ; Gu, Wenjin

  • Author_Institution
    Dept. of Autom. Control, Naval Aeronaut. Eng. Inst., Yantai, China
  • Volume
    1
  • fYear
    2004
  • fDate
    6-9 Dec. 2004
  • Firstpage
    778
  • Abstract
    A scheme of integrated guidance/autopilot design for STT missile against maneuvering targets on the sea is proposed. Three channels independence design idea is adopted. Firstly, an integrated guidance/autopilot model of the yaw plane is formulated and the guidance/control law is designed based on the backstepping idea and variable structure control theory. Secondly, control laws are proposed for the height and roll angle, so that when a missile has the capability to hit the target on the yaw plane, and the height approaches zero as the distance between the missile and target on the yaw plane tends to zero, the missile will hit the target. Finally, to verify the effectiveness and rightness of the integrated design scheme, a simulation of some anti-vessel missile against high maneuvering targets was made and the results show that a high accuracy of hitting a target can be achieved.
  • Keywords
    attitude control; control system synthesis; marine vehicles; missile guidance; position control; STT missile; anti-vessel missiles; backstepping; guidance/control law; height control; integrated guidance/autopilot scheme; maneuvering sea targets; roll angle control; three channel independence design; variable structure control theory; yaw plane; Acceleration; Aerospace engineering; Backstepping; Control theory; Coordinate measuring machines; Equations; Missiles; Navigation; Sea measurements; Virtual manufacturing;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control, Automation, Robotics and Vision Conference, 2004. ICARCV 2004 8th
  • Print_ISBN
    0-7803-8653-1
  • Type

    conf

  • DOI
    10.1109/ICARCV.2004.1468926
  • Filename
    1468926