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)
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    References(2)

    [4] [4] MIN C, MA T H, HE J, et al. Study on the attitude control for high-speed rotary missile based on neural networks[C]//International Conference on Electronics and Optoelectronics (ICEOE), IEEE, 2011: V3-428-V3-430.

    [5] [5] LI H, FAN Y, LI F Y, et al. Missile attitude control in a large flight envelope based on the linear active distur-bance rejection control approach[C]//Guidance, Naviga-tion and Control Conference, IEEE, 2015: 1219-1223.

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    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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    Paper Information

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    Received: Jan. 13, 2017

    Accepted: --

    Published Online: Jan. 22, 2021

    The Author Email:

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

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