• Journal of Atmospheric and Environmental Optics
  • Vol. 18, Issue 3, 235 (2023)
ZHANG Quan1, LI Xin1、*, WEI Wei1, LIU Enchao1, ZHANG Yanna1, HUANG Xionghao1、2, CHEN Shengli1、2, KANG Zhuhai1、2, and ZHENG Xiaobing1
Author Affiliations
  • 1Key Laboratory of Optical Calibration and Characterization, Anhui Institute of Optics and Fine Mechanics, HFIPS, Chinese Academy of Sciences, Hefei 230031, China
  • 2University of Science and Technology of China, Hefei 230026, China
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    DOI: 10.3969/j.issn.1673-6141.2023.03.005 Cite this Article
    Quan ZHANG, Xin LI, Wei WEI, Enchao LIU, Yanna ZHANG, Xionghao HUANG, Shengli CHEN, Zhuhai KANG, Xiaobing ZHENG. Design of BRDF measurement system based on multi-rotor UAV[J]. Journal of Atmospheric and Environmental Optics, 2023, 18(3): 235 Copy Citation Text show less
    Compositions of multi-rotor UAV
    Fig. 1. Compositions of multi-rotor UAV
    Photo of multi-rotor UAV
    Fig. 2. Photo of multi-rotor UAV
    Spectroscopic principle diagram of flat-field concave grating
    Fig. 3. Spectroscopic principle diagram of flat-field concave grating
    Visible-short-wave infrared spectrometer. (a) 3D modeling; (b) physical photo
    Fig. 4. Visible-short-wave infrared spectrometer. (a) 3D modeling; (b) physical photo
    Stray light path of VNIR unit
    Fig. 5. Stray light path of VNIR unit
    Stray light path of SWIR unit
    Fig. 6. Stray light path of SWIR unit
    UAV BRDF measurement route hierarchy
    Fig. 7. UAV BRDF measurement route hierarchy
    Measurement of polygonal route by UAV BRDF
    Fig. 8. Measurement of polygonal route by UAV BRDF
    BRDF reflectivity data of Dunhuang test site
    Fig. 9. BRDF reflectivity data of Dunhuang test site
    BRF distribution of Dunhuang test site in 2019. (a) λ = 554 nm; (b) λ = 857 nm; (c) λ = 1242 nm
    Fig. 10. BRF distribution of Dunhuang test site in 2019. (a) λ = 554 nm; (b) λ = 857 nm; (c) λ = 1242 nm
    TypeParameter
    Load weight/kg10
    Hover precision/mVertical: ±0.5, horizontal: ±1.5
    Maximum Angle/(°)25
    Maximum wind speed/(m·s-1)8
    Maximum level flying speed/(m·s-1)12 (Windless environment)
    Operating environment temperature/℃-10~40
    Table 1. Technical parameters of multi-rotor UAV
    TypeParameter
    Weight/kg2.77
    Load weight/kg4.5
    Operating environment temperature/℃-15~50
    Angle jitter/(°)±0.02
    Table 2. Technical parameters of cradle head
    TypeParameter
    Spectral range/nm400~1000
    F#2.2
    Scribed line density/(gr·mm-1)310.5
    Spectral width/(k·mm-1)12.7
    Average dispersion(nm·mm-1)47.2
    Table 3. Grating parameters of VNIR unit
    TypeParameter
    Spectral range/nm850~1700
    F#2.2
    Scribed line density/(gr·mm-1)221
    Spectral width(k·mm-1)12.7
    Average dispersion(nm·mm-1)67
    Table 4. Grating parameters of SWIR unit
    Quan ZHANG, Xin LI, Wei WEI, Enchao LIU, Yanna ZHANG, Xionghao HUANG, Shengli CHEN, Zhuhai KANG, Xiaobing ZHENG. Design of BRDF measurement system based on multi-rotor UAV[J]. Journal of Atmospheric and Environmental Optics, 2023, 18(3): 235
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