• Electronics Optics & Control
  • Vol. 24, Issue 12, 1 (2017)
HE Hua-feng, HAN Cong-cong, and YANG Zong-hao
Author Affiliations
  • [in Chinese]
  • show less
    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
    References

    [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] 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.

    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