• DocumentCode
    551207
  • Title

    Differential flatness based control of Glide-reentry anti-vessel missile engineless part

  • Author

    Li Congying ; Han Lei ; Xu Xiaofei ; Yu Jinyong

  • Author_Institution
    7th Dept., Naval Aeronaut. Eng. Inst., Yantai, China
  • fYear
    2011
  • fDate
    22-24 July 2011
  • Firstpage
    807
  • Lastpage
    811
  • Abstract
    Nonlinear inverse dynamic controller based on differential flatness was designed for Glide-reentry anti-vessel missile terminal engineless part. Aerodynamic data was processed to make the missile model flat. Brake rudder was introduced to control terminal energy and fulfill the requirement of flatness.
  • Keywords
    aerodynamics; control system synthesis; missile control; nonlinear control systems; vehicle dynamics; aerodynamic data; brake rudder; differential flatness based control; glide-reentry antivessel missile engineless part; nonlinear inverse dynamic controller; terminal energy; Aerodynamics; Atmospheric modeling; Conferences; Electronic mail; Missiles; Nonlinear systems; Trajectory; Anti-Vessel Missile; Differential Flatness; Glide-Reentry; Nonlinear Inverse Dynamic;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Conference (CCC), 2011 30th Chinese
  • Conference_Location
    Yantai
  • ISSN
    1934-1768
  • Print_ISBN
    978-1-4577-0677-6
  • Electronic_ISBN
    1934-1768
  • Type

    conf

  • Filename
    6001552
    • Link To Document
    https://search.isc.ac/dl/search/defaultta.aspx?DTC=49&DC=551207