Electronics Optics & Control, Volume. 24, Issue 12, 1(2017)

Modeling and Simulation of Ballistic Trajectory Direction Change in Boost Phase of Missile

HE Hua-feng... HAN Cong-cong and YANG Zong-hao |Show fewer author(s)
Author Affiliations
  • [in Chinese]
  • show less

    If the missile is converted to attack another target once it has aimed at one target, the repositioning will have a very serious impact on maneuvering capability of the missile. Based on the basic principle of the firing direction change of the missile body, this paper establishes a model of missile firing direction change, presents a method to realize the change by rolling of missile body in the boost phase. The simulation results show that: 1) The model can achieve the direction change in boost phase of ballistic missile; 2) The designed simulation system has certain anti-interference capability, and rolling angle command tracking effect is fine;and 3) The missile can fly steadily.

    Tools

    Get Citation

    Copy Citation Text

    HE Hua-feng, HAN Cong-cong, YANG Zong-hao. Modeling and Simulation of Ballistic Trajectory Direction Change in Boost Phase of Missile[J]. Electronics Optics & Control, 2017, 24(12): 1

    Download Citation

    EndNote(RIS)BibTexPlain Text
    Save article for my favorites
    Paper Information

    Category:

    Received: Jan. 13, 2017

    Accepted: --

    Published Online: Jan. 22, 2021

    The Author Email:

    DOI:10.3969/j.issn.1671-637x.2017.12.001

    Topics