Acta Optica Sinica, Volume. 43, Issue 18, 1899902(2023)

Comparison and Analysis of Payloads Performance for Active and Passive Spaceborne Atmospheric Detection

Jingsong Wang1,3 and Dong Liu1,2、*
Author Affiliations
  • 1Key Laboratory of Atmospheric Optics, Anhui Institute of Optics and Fine Mechanics, Hefei Institutes of Physical Science, Chinese Academy of Sciences, Hefei 230031, Anhui, China
  • 2Advanced Laser Technology Laboratory of Anhui Province, Hefei 230037, Anhui, China
  • 3Science Island Branch of Graduate School, University of Science and Technology of China, Hefei 230026, Anhui, China
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    Figures & Tables(13)
    ICESat (left) and GLAS (right) models[25]
    CALIOP payload (left) and its functional block diagram (right)[39]
    CATS on ISS (left) [54] in three working modes (right) [56]
    ADM-Aeolus detection system schematic[59]
    DQ-1 (left) and ACDL system functional diagram (right) [69]
    CM-1 operating in orbit[70]
    Schematic diagram of IPDA method[86]
    • Table 1. Main international spaceborne Lidar payload

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      Table 1. Main international spaceborne Lidar payload

      Platform Lidar payloadSSD LITECALIPSO CALIOPICESat GLASICESat-2 ATLASISS CATSAeolus ALADINDQ-1 ACDLCM-1 CASAL
      Total satellite weight /kg5879701514140026002936
      Launch year19942006200320182015201820222022
      Type of orbitNon-solar synchronousSolar synchronousNon-solar synchronousNon-solar synchronousNon-solar synchronousSolar synchronousSolar synchronousSolar synchronous
      Orbital altitude /km260705600500405320705506
      Orbital inclination /(°)5798.2949251.649798.13597.421
      Repetition period /d169191375159
      Design life10 d3 a3 a3 a0.5 a3 a3 a8 a
      Target of detectionClouds,aerosols,etc.Clouds,aerosols,etc.Ice,terrain,clouds,aerosols,etc.Ice,terrain,vegetation,etc.Clouds,aerosols,etc.Wind fields,clouds,aerosols,etc.CO2,clouds,aerosols,etc.Vegetation biomass,chlorophyll fluorescence,aerosol,etc.
    • Table 2. Main technical parameters of international spaceborne Lidars

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      Table 2. Main technical parameters of international spaceborne Lidars

      PayloadSpatial resolutionTransmitting unitReceiving unit
      VerticalLevelLaserWavelengthSingle pulse energyRepeat frequencyPulse widthDivergence angleTelescope diameterField of viewPhotovoltaic conversion
      LITE35 m740 mNd:YAG355,532,and 1064 nm

      500 mJ

      @532 nm

      500 mJ

      @1064 nm

      160 mJ@355 nm

      10 Hz1 mrad1 m

      PMT@

      355 nm,532 nm

      APD@

      1064 nm

      CALIOP30 m333 mNd:YAG532 and 1064 nm

      110 mJ@532 nm

      110 mJ@1064 nm

      20.16 Hz20 ns0.1 mrad1 m0.13 mrad

      PMT

      @532 nm

      APD@

      1064 nm

      GLAS

      Course 170 m

      Lateral(maximum)15000 m Lateral(minimum)

      2500 m

      Nd:YAG532 and 1064 nm

      75 mJ@1064 nm

      35 mJ@532 nm

      40 Hz5 ns0.11 mrad1 m

      0.475 mrad@1064 nm

      0.15 mrad @532 nm

      SiAPD
      ATLAS

      Course 90 m

      Lateral(two strong or two weak)3300 m

      Lateral(strong and weak)

      2500 m

      Nd:YVO4532 nm

      Strong:0.12 mJ

      Weak:0.04 mJ

      10 KHz1 ns0.024 mrad0.8 m83 μradPMT
      CATS25 m15 mNd:YVO4355,532,and 1064 nm2 mJ4 kHz30 ns0.03 mrad0.6 m110 mrad@+/-0.5°

      PMT@355 nm,532 nm

      APD@1064 nm

      ALADIN0.25-2.00 km87 kmNd:YAG355 nm150 mJ100 Hz15 ns12 μrad1.5 m22 μradCCD
      ACDL30 m337.5 mNd:YAG532,1064,and 1572 nm

      ≥150 mJ@532 nm

      ≥110 mJ@1064 nm

      ≥75 mJ@1572 nm

      20 Hz@1572 nm

      40 Hz@532 nm

      40 Hz@ 1064 nm

      ≤50 ns@532 nm

      ≤50 ns@1064 nm

      ≤15 ns@1572 nm

      100 μrad1 m0.2 mrad

      PMT

      @532 nm

      APD@

      1572 nm

      APD@

      1064 nm

      CASAL≤30 m532 and 1064 nm

      73 mJ@1064 nm

      110 mJ@1064/532 nm

      40 Hz

      40-60 μrad

      @1064 nm

      ≤200 μrad @1064/532 nm

      1 mAPD
      ACENd:YAG355,532,and 1064 nm1.5 m

      PMT

      @355 nm,532 nm

      APD@

      1064 nm

      ATLID40 mNd:YAG1064 nm100 mJ100 Hz20 ns125 μrad0.6 m

      APD@

      1064 nm

      EarthCARE

      100 m@

      0-20 km

      500 m@20-40 km

      282 mNd:YAG355 nm38 mJ51 Hz25 ns45 μrad0.62 m75 μrad

      PMT

      @355 nm

      MERLINNd:YAG1645 nm9 mJ20 Hz20-30 ns0.69 m

      APD

      @1645 nm

      A-SCOPE

      Nd:YAG

      Ho-Tm:YAG

      1.57/

      2.05 μm

      50/55 mJ50 Hz

      0.435/

      0.2 mrad

      1 m0.476/0.22 mradAPD
      ASCENDS1572 nm10 kHz1.5 mAPD
    • Table 3. Comparison of cloud remote sensing satellite payload performance

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      Table 3. Comparison of cloud remote sensing satellite payload performance

      PayloadSatelliteActive and passiveAdvantageDisadvantage
      MERSI-II AGRIFengyunPassiveWith mature development,remote sensing instruments and inversion algorithms are diverse,and Fengyun satellite can form a network detectionDepending on sunlight,the temporal and spatial resolution is insufficient,the difference of the results of different algorithms is questionable,and the inversion effect is poor for complex cloud scenes
      DPCGF-5
      MODISTerra/Aqua
      AHIHimawari
      CPRCloudSatActiveMicrowave radar can detect the vertical structure of thick clouds due to its strong penetration ability. Spaceborne Lidar has obvious advantages in retrieving cloud top height and high detection accuracy,and has unique advantages in macro and micro parameters of thin cloudsMicrowave radar has low spatial resolution,low sensitivity to small-scale clouds,and does not have the detection ability from the ground to an altitude of 1 km,and the limited penetration ability of lidar makes it difficult to retrieve the height of the cloud base,and has limitations for the detection of thick clouds. The sky signal to noise ratio is low
      CALIOPCALIPSO
      ACDLDQ-1
    • Table 4. Comparison of atmospheric aerosol remote sensing satellite payload performance

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      Table 4. Comparison of atmospheric aerosol remote sensing satellite payload performance

      PayloadSatelliteActive and passiveAdvantageDisadvantage
      AVHRRNOAAPassiveMulti-spectral,multi-angle and polarization means,algorithms and instruments are diverse,the space coverage is large,and the retrievable aerosol parameters are numerousDepending on sunlight,the spatial and temporal resolution is insufficient,the detection accuracy is limited,and the aerosol profile information cannot be provided
      DPCGF-5
      MODISTerra/Aqua
      MISRTerra
      GLASICESatActiveIt can detect aerosol by quantitative remote sensing,with high spatial and temporal resolution,provide global aerosol vertical structure and high detection accuracy. ACDL's HSRL system based on iodine filter can obtain aerosol information with higher accuracy without introducing Lidar ratioCALIOP needs to assume Lidar ratios,increasing sources of error
      CALIOPCALIPSO
      CATSISS
      ACDLDQ-1
    • Table 5. Comparison of greenhouse gas remote sensing satellite payload performance

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      Table 5. Comparison of greenhouse gas remote sensing satellite payload performance

      PayloadSatelliteActive and passiveAdvantageDisadvantage
      SCIAMACHYEnvisat-1PassiveVarious technologies,including Fourier interferometry,grating spectroscopy and space heterodyne spectroscopy technology,strong specialization,and there are specialized passive satellites to detect greenhouse gases,and a variety of observation modes,including nadir,flare,calibration,and targetData validity is limited by clouds,aerosols,and latitude zones,surface reflectivity and atmospheric component scattering affect detection accuracy,and time and space are limited by night and north and south poles
      TANSO-FTSGOSAT
      3-channel grating spectrometerOCO
      ACGSTANSAT
      GMIGF-5
      ACDLDQ-1ActiveHigh detection accuracy,CO2 detection is expected to achieve 1×10-6 accuracy,not easily affected by clouds and aerosols,can achieve all day observation,fill the gap of CO2 night observation,does not depend on the sun angle,the observation area covers the poles to achieve full latitude observationThe laser has high requirements and is difficult to develop,and the atmospheric parameters affect the high-precision inversion of greenhouse gases
    • Table 6. Comparison of atmospheric wind field remote sensing satellite payload performance

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      Table 6. Comparison of atmospheric wind field remote sensing satellite payload performance

      PayloadSatelliteActive and passiveAdvantageDisadvantage
      SEVIRIIMSGPassiveVarious detection techniques. The detection range is wide,including the atmospheric wind field in the mesosphere and most of the thermosphere height range. In the observation of tropospheric wind field,spaceborne passive remote sensing has reached the level of operational observationThe detection accuracy and spatial resolution are worse than that of active remote sensing
      WINDIIUARS
      HRDIUARS
      MIGHTIICON
      ALADINADM-AeolusActiveIt can provide the vertical profile of the global atmospheric wind field with high precision and high spatio-temporal resolution,and is one of the best means to obtain the three-dimensional global atmospheric wind field. There are many wind measurement systems that can be developed,and the development potential is greatThe detection range is small,and the atmospheric wind profile in the global range of 0-25 km is detected. At present,there is only one kind of ALADIN,the system is single,and there is no Lidar wind measurement satellite in our country
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    Jingsong Wang, Dong Liu. Comparison and Analysis of Payloads Performance for Active and Passive Spaceborne Atmospheric Detection[J]. Acta Optica Sinica, 2023, 43(18): 1899902

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    Paper Information

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    Received: Jun. 19, 2023

    Accepted: Aug. 11, 2023

    Published Online: Sep. 14, 2023

    The Author Email: Dong Liu (dliu@aiofm.cas.cn)

    DOI:10.3788/AOS231153

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