• Electronics Optics & Control
  • Vol. 24, Issue 12, 1 (2017)
HE Hua-feng, HAN Cong-cong, and YANG Zong-hao
Author Affiliations
  • [in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2017.12.001 Cite this Article
    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 Copy Citation Text show less

    Abstract

    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.
    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
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