• DocumentCode
    572508
  • Title

    3D guidance for vertical impact on non-stationary targets

  • Author

    Zhang, Jinpeng ; Cao, Youliang ; Song, Xiaona ; Zhang, Minglian ; Shen, Gongzhang

  • Author_Institution
    Sci. & Technol. on Aircraft Control Lab., Beihang Univ., Beijing, China
  • fYear
    2012
  • fDate
    15-17 Aug. 2012
  • Firstpage
    272
  • Lastpage
    276
  • Abstract
    A new three-dimensional guidance law with high impact angle constraints used for striking ground moving targets is designed based on back-stepping control approach. The kinematics between the missile and the target are established in line-of-sight (LOS) frame. To ensure the required impact angle and small miss distance, two step controllers are designed based on Lyapunov method. The first step controller guarantees the LOS angle in vertical plane to converge to the desired angle. The second step controller can stabilize the overall system while maintaining minimum LOS rate, and thus the smallest miss distance can be achieved indirectly. Simulation results illustrate the efficiency.
  • Keywords
    Lyapunov methods; control system synthesis; missile guidance; 3D guidance; LOS angle; Lyapunov method; back-stepping control approach; designed controller; ground moving targets; high impact angle constraints; line-of-sight frame; miss distance; missile-target kinematics; nonstationary targets; step controller; system stabilization; three-dimensional guidance law; vertical impact; Acceleration; Backstepping; Equations; Missiles; Simulation; Trajectory; Vectors; Air-to-air missiles; Back-stepping control; guidance law; high impact angle; maneuvering target;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Automation and Logistics (ICAL), 2012 IEEE International Conference on
  • Conference_Location
    Zhengzhou
  • ISSN
    2161-8151
  • Print_ISBN
    978-1-4673-0362-0
  • Electronic_ISBN
    2161-8151
  • Type

    conf

  • DOI
    10.1109/ICAL.2012.6308210
  • Filename
    6308210