• DocumentCode
    2195869
  • Title

    Pole placement controller design for relaxed stable stability missile

  • Author

    Zhengyu, Guo ; Xiaogeng, Liang

  • Author_Institution
    Luoyang Opto-Electro Technol. Dev. Center, Luoyang, China
  • fYear
    2011
  • fDate
    9-11 Sept. 2011
  • Firstpage
    1577
  • Lastpage
    1580
  • Abstract
    Relaxed Stable Stability is a new way to rise the flying speed, distance and maneuverability of missile. The focus of this paper is on the pole placement controller design for RSS missile. First, a concise introduction of RSS and pole placement controller and the vertical direction perturbation equations are described. Then a controller is developed. By using this, we simulate a missile model. Simulation results as well as stability analysis of RSS missile demonstrate the validity of the proposed scheme.
  • Keywords
    control system synthesis; missile control; perturbation techniques; pole assignment; stability; RSS missile; flying speed; missile distance; missile maneuverability; missile model; perturbation equation; pole placement controller design; relaxed stable stability missile; Aerodynamics; Mathematical model; Missiles; Simulation; Stability analysis; State feedback; Controller Design; Pole Placement Controller; Relaxed Stable Stability Missile;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Electronics, Communications and Control (ICECC), 2011 International Conference on
  • Conference_Location
    Ningbo
  • Print_ISBN
    978-1-4577-0320-1
  • Type

    conf

  • DOI
    10.1109/ICECC.2011.6067734
  • Filename
    6067734