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Takeoff/landing controller design for a tilted bi-rotor aircraft
Micro/Nano Technology and Fine Mechanics | 更新时间：2026-02-24

    • Takeoff/landing controller design for a tilted bi-rotor aircraft

    • “The research progress in the field of takeoff and landing control of tiltrotor bipotor aircraft was introduced. Experts designed a takeoff and landing controller and conducted flight verification experiments, providing an effective solution to the stability problem of aircraft takeoff and landing.”
    • Optics and Precision Engineering   Vol. 34, Issue 4, Pages: 599-610(2026)

    • DOI：10.37188/OPE.20263404.0599    

      CLC： TP394.1;TH691.9
    • CSTR：32169.14.OPE.20263404.0599    

    • Received：20 September 2025，

      Revised：2025-11-20，

      Published：25 February 2026

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  • WANG Tianqi,YU Hai.Takeoff/landing controller design for a tilted bi-rotor aircraft[J].Optics and Precision Engineering,2026,34(04):599-610.

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