Acta Optica Sinica, Volume. 45, Issue 18, 1828003(2025)

Application of Space Optical Payloads in Near-Earth Asteroid Defense (Invited)

Changning Huang*, Yongfu Hu, Jianfu Wu, and Yan Chen
Author Affiliations
  • Beijing Institute of Space Mechanics and Electricity, Beijing 100094, China
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    Figures & Tables(4)
    Exploded-view drawing of DRACO with major components labeled[6]
    On-orbit imaging of the DRACO camera[13]
    • Table 1. Technical specifications and inheritance of optical payloads

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      Table 1. Technical specifications and inheritance of optical payloads

      Mission/payloadParameterInheritanceImprovementAchievement
      DART/DRACO cameraAngular resolution is 2.48 µrad;aperture is 208 mm; field of view is 0.29°; magnitude detection is 14.5New Horizons, Lucy/LORRIChanged CCD to CMOS; global/rolling shutter dual-mode operation; integrated SMART Nav autonomous navigation algorithm; optimized adaptability to low-temperature conditions [(-85±5) ℃]Autonomous guidance achieved cm-level impact point positioning for 160 m-class asteroids (1σ error ±68 cm); obtained the size and quantity distribution of boulders on asteroids
      Hera/AFC cameraSpectral band is 370‒1100 nm;angular resolution is 94.1 µrad; field of view is 5.5°×5.5°Astrohead camerasImproved close-range imaging resolution (10 cm/pixel); balanced dual-mode functions of navigation and imagingSupports 3D shape reconstruction and accurate volume calculation of binary systems; determines density and internal structure by combining mass data
      Hera/TIRI thermal infrared imager7‒14 μm mid-infrared spectral band; resolution is 5 m@20 km;field of view is 13°×10°;temperature measurement range is 150‒400 K; accuracy is 3 KHayabusa 2/ TIRResolution increased by 4 times; expanded spectral band width; sensor changed to Lynred Pico 1024 Gen 2Retrieves thermal inertia through surface temperature distribution, infers thermophysical properties such as roughness and porosity, and helps understand the Yarkovsky/YORP effect[10]
      Hera/HyperScout H imaging spectrometerSpectral band is 665‒975 nm; angular resolution is 133 µrad; field of view is 16°×8°; number of spectral bands is 25HyperScout-2

      Simplified the infrared spectral band;

      reduced the number of spectral bands from 45 to 25; lightweight design

      Detects post-impact surface mineral changes, impact crater space weathering effects, and ejecta deposition to support impact effect evaluation
      Hera/ASPECT hyperspectral imagerFour-channel independent measurement (visible light, two near-infrared, one short-wave infrared); achieves 20‒40 nm spectral resolution using a tunable Fabry-Perot interferometer (FPI)CubeSat Aalto-1/ AASIExpanded the spectral band;optimized the resolutionExplores the surface mineral composition of asteroids, characterizes asteroid volatiles and dust particles, and assists in determining their composition
      LICIACube/LEIA, LUKEWide-field and narrow-field cameras respectively; panchromatic, color; resolution is 1.5‒5 m/pixel; field of views are 2.06° and 10°CubeSat general payloadAcquire images of the unimpacted side of the asteroid and videos of the dynamic evolution of ejecta respectively
    • Table 2. Comparison of optical payload technologies

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      Table 2. Comparison of optical payload technologies

      PayloadMain functionPerformanceInheritanceInnovation and shortcoming
      High-resolution cameraAcquire physical characteristics such as asteroid shape and conduct plume monitoring and evaluationResolution is 0.1 m@30 kmvideo/imaging modesLunar exploration, Tianwen-1 high-resolution cameraEquipped with a focusing mechanism to adapt to imaging at distances from 2 km to 30000 km, which increases weight and power consumption;video mode captures the dynamics of plume
      Multispectral cameraUsed for the study of surface topography and material properties480‒1000 nm; number of spectral bands ≥8Lunar exploration, Tianwen-1/2 spectral camera

      Differences in technical systems;

      multispectral camera is implemented using filter wheels and have mechanical components

      Visible-infrared spectrometerAcquire high-resolution spectral data of the visible to infrared bands on the asteroid surface400‒1000 nm; number of spectral bands ≥256Lunar exploration, Tianwen-1/2 multispectralLarge number of spectral bands, requiring further lightweighting
      Thermal radiation spectrometerDetect the thermal radiation characteristics of the asteroid5‒50 μm; temperature measurement accuracy is ±2 KTianwen-2 thermal radiation spectrometerMulti-source data fusion improves the accuracy of thermal inertia retrieval
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    Changning Huang, Yongfu Hu, Jianfu Wu, Yan Chen. Application of Space Optical Payloads in Near-Earth Asteroid Defense (Invited)[J]. Acta Optica Sinica, 2025, 45(18): 1828003

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    Paper Information

    Category: Remote Sensing and Sensors

    Received: Jul. 10, 2025

    Accepted: Aug. 28, 2025

    Published Online: Sep. 19, 2025

    The Author Email: Changning Huang (2313080520@qq.com)

    DOI:10.3788/AOS251446

    CSTR:32393.14.AOS251446

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