• Chinese Journal of Ship Research
  • Vol. 19, Issue 1, 272 (2024)
Jiejie KONG1,2, Jianyao WANG1,2, and Hongdong WANG1,2
Author Affiliations
  • 1State Key Laboratory of Ocean Engineering, Shanghai Jiao Tong University, Shanghai 200240, China
  • 2Key Laboratory of Marine Intelligent Equipment and System of Ministry of Education, Shanghai Jiao Tong University, Shanghai 200240, China
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    DOI: 10.19693/j.issn.1673-3185.02990 Cite this Article
    Jiejie KONG, Jianyao WANG, Hongdong WANG. A new multi-rotor UAV landing device and safety boundary assessment method[J]. Chinese Journal of Ship Research, 2024, 19(1): 272 Copy Citation Text show less
    [in Chinese]
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    参数数值
    轴距/mm450
    结构重量/g1 200
    机身尺寸/cm35×45×23
    桨尺寸/cm22.86
    Table 1. Parameters for Dajiang F450 UAV
    着舰网参数数值V形足参数数值
    网孔尺寸/mm40×40密度/(kg·m–3)1116.7
    丝径尺寸/mm2杨氏模量/MPa1 827
    材质泊松比0.395
    密度/(kg·m–3)7 801单个重量/g24.47
    杨氏模量/MPa2.07×105
    泊松比0.29
    Table 2. Dimensional parameters of the "V-foot–net" device
    横摇角/(º)“V形足–网”装置普通着舰装置
    临界周期/s稳定时间/s临界周期/s稳定时间/s
    10.10.410.30.65
    20.10.400.30.76
    30.10.410.41.16
    40.10.490.42.22
    50.10.600.51.53
    60.20.480.62.11
    70.20.480.72.15
    80.20.470.82.12
    90.20.500.92.09
    100.30.561.01.98
    110.30.851.12.19
    120.50.851.22.32
    130.51.101.32.24
    140.61.311.42.35
    150.61.011.52.46
    160.71.101.62.6
    170.71.501.72.48
    180.71.561.72.25
    190.81.831.92.75
    200.82.162.03.38
    Table 3. Simulation results