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    Journals >Electronics Optics & Control >Volume 26 >Issue 3 >Page 108 > Article
    • Electronics Optics & Control
    • Vol. 26, Issue 3, 108 (2019)
    Modeling of Rotational Inertia for Tilting Three-Rotor UAV
    ZOU Ming-hu1 and ZHANG Fei2
    Author Affiliations
  • 1[in Chinese]
  • 2[in Chinese]
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    DOI: 10.3969/j.issn.1671-637x.2019.03.022 Cite this Article
    ZOU Ming-hu, ZHANG Fei. Modeling of Rotational Inertia for Tilting Three-Rotor UAV[J]. Electronics Optics & Control, 2019, 26(3): 108 Copy Citation Text show less
    References

    [4] NOTARSTEFANO G,HAUSER J.Modeling and dynamic exploration of a tilt-rotor VTOL aircraft［C］//The 8th IFAC Symposium on Nonlinear Control Systems, Bologna, 2010: 119-124.

    [5] BOLKCOM C.V-22 osprey tilt-rotor aircraft［R］.Washington:CRS Report for Congress,2004.

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    ZOU Ming-hu, ZHANG Fei. Modeling of Rotational Inertia for Tilting Three-Rotor UAV[J]. Electronics Optics & Control, 2019, 26(3): 108
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