• DocumentCode
    1677096
  • Title

    Guidance law for a modern munition

  • Author

    Park, Woosung ; Yun, Joongsup ; Ryoo, Chang-Kyung ; Kim, Yongho

  • Author_Institution
    Dept. of Aerosp. Eng., Inha Univ., Incheon, South Korea
  • fYear
    2010
  • Firstpage
    2376
  • Lastpage
    2379
  • Abstract
    While the PN (Proportional Navigation) guidance is known generally in the study of the missile guidance, there are not broadly known guidance laws for the munitions. Some guidance laws like the Impact Point Prediction, Modified Proportional Navigation Guidance, and Neural Network are considered currently. In this paper, we suggest the new guidance law of using the sensitivity. The sensitivity is a value about the relationship between the variation of velocity and the impact point error. Finally, we simulate the trajectory correction of the munition through this guidance law.
  • Keywords
    attitude control; position control; weapons; impact point prediction; missile guidance; munition guidance; neural network; proportional navigation guidance; sensitivity law; trajectory correction simulation; Acceleration; Firing; Mathematical model; Navigation; Sensitivity; Trajectory; Weapons; Guidance Law; Guided Munition; Predictor; Sensitivity;
  • fLanguage
    English
  • Publisher
    ieee
  • Conference_Titel
    Control Automation and Systems (ICCAS), 2010 International Conference on
  • Conference_Location
    Gyeonggi-do
  • Print_ISBN
    978-1-4244-7453-0
  • Electronic_ISBN
    978-89-93215-02-1
  • Type

    conf

  • Filename
    5669937