• Electronics Optics & Control
  • Vol. 28, Issue 7, 103 (2021)
WANG Cheng1, WANG Xugang2, and ZHU Yin3
Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
  • 3[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2021.07.021 Cite this Article
    WANG Cheng, WANG Xugang, ZHU Yin. Effect of Projectile Rolling Speed on Its Control Coupling and the Decoupling Method[J]. Electronics Optics & Control, 2021, 28(7): 103 Copy Citation Text show less
    References

    [6] LESTAGE R.Analysis of control and guidance of rolling missiles with a single plane of control fins[C]//AIAA Guidance,Navigation,and Control Conference and Exhibit, 2000:14-17.

    [7] LI K,YANG S,ZHAO L.Stability of spinning missiles with an acceleration autopilot[J].Journal of Guidance,Control and Dynamics,2012,35(3):774-786.

    [9] WANG Z Y,CHANG S J.Impact point prediction and analysis of lateral correction of two-dimensional trajectory correction projectiles[J].Defence Technology,2013,9(1):48-52.

    WANG Cheng, WANG Xugang, ZHU Yin. Effect of Projectile Rolling Speed on Its Control Coupling and the Decoupling Method[J]. Electronics Optics & Control, 2021, 28(7): 103
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