Lunar calibration method through attitude maneuver of low-earth-orbit and high-resolution remote sensing satellites

Jun ZHU; Yong-chang LI; Zhao-guang BAI; Chun-ling LU; Kai-lin FU; Xin-bai MAO; Lu ZHANG

doi:10.37188/OPE.20202809.1913

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Lunar calibration method through attitude maneuver of low-earth-orbit and high-resolution remote sensing satellites

Modern Applied Optics | 更新时间：2020-09-28

- Lunar calibration method through attitude maneuver of low-earth-orbit and high-resolution remote sensing satellites
- Optics and Precision Engineering Vol. 28, Issue 9, Pages: 1913-1923(2020)
- 作者机构：
  
  1.航天东方红卫星有限公司, 北京 100094
  2.国家卫星气象中心, 北京 100081
- 作者简介：
- 基金信息：
- DOI：10.37188/OPE.20202809.1913
  CLC： V474
- Received：15 January 2020，
  
  Revised：13 March 2020，
  
  Accepted：13 March 2020，
  
  Published：25 September 2020
- 稿件说明：
移动端阅览
Jun ZHU, Yong-chang LI, Zhao-guang BAI, et al. Lunar calibration method through attitude maneuver of low-earth-orbit and high-resolution remote sensing satellites[J]. Optics and precision engineering, 2020, 28(9): 1913-1923.
DOI：

Jun ZHU, Yong-chang LI, Zhao-guang BAI, et al. Lunar calibration method through attitude maneuver of low-earth-orbit and high-resolution remote sensing satellites[J]. Optics and precision engineering, 2020, 28(9): 1913-1923. DOI： 10.37188/OPE.20202809.1913.

摘要

月球作为光谱特性稳定、光强在探测器动态范围内的理想定标源，利用月球进行卫星在轨对月定标是提高辐射定标效率、监测探测器成像稳定性的重要手段之一。针对低轨高分辨率遥感卫星，提出了一种姿态机动对月定标方法，包括对月定标时机选择、对月定标卫星姿态规划以及载荷成像参数选取等技术。并基于某在轨运行的低轨光学遥感卫星成功开展了15次对月定标实验，卫星姿态角速度为0.06（°）/s，载荷积分时间为0.293 8 ms，月相角覆盖-79.872°~89.236°。实验结果表明，卫星姿态实际执行情况符合设计的对月定标卫星姿态规划流程，且该对月定标方法具有很高的观测效率，仅耗时1 500 s，不会影响卫星正常的对地观测任务；地面获取的15幅月球图像纹理清晰、稳定，对月空间分辨率优于1.18 km，图像DN值分布层次感较好；计算得出的月球辐照度分布趋势与国际上ROLO（Robotic Lunar Observatory）模型公布的趋势一致。实验结果验证了提出的对月定标方法的正确性及合理性，同时实现了中国首次低轨高分辨率遥感卫星姿态机动对月球多月相角观测，可为长期监测卫星探测器的成像稳定性和大量积累对月定标数据、建立中国自主可控的月球辐射模型提供可靠依据。

Abstract

As an ideal calibration source

the moon has stable spectral characteristics and light intensity within the dynamic range of the detector. Thus

lunar calibration on-orbit is one of the important means to improve the efficiency of radiometric calibration and monitor the imaging stability of remote sensing satellites. Targeting low earth orbit and high-resolution remote sensing satellites

an on-orbit lunar calibration method

which includes imaging time

satellite attitude

imaging parameters of lunar observation

etc.

is proposed in this paper. Lunar observation experiments on a low-orbit optical remote sensing satellite were successfully conducted 15 times in July

2019

under the conditions of satellite attitude angular velocity of 0.06 (°)/s and integration time of 0.293 8 ms. The lunar phase angle covered the range of -79.872° to 89.236°. The results suggest that the satellite attitude of the actual implementation is in accordance with that of the design. Moreover

the lunar calibration method has high observation efficiency

which takes only 1 500 s and will not affect the normal earth observation mission. Furthermore

the texture of 15 acquired images of the moon has a better distribution hierarchy of image DN value

and the spatial resolution is better than 1.18 km. The calculated lunar irradiance distribution trend is consistent with that of the RObotic Lunar Observatory (ROLO) model published internationally. The experimental results verified the correctness and rationale of the proposed method. Multiple lunar phase angle observation has been realized for the first time in China though the attitude maneuver of a low-orbit remote sensing satellite

which can provide a reliable basis for long-term monitoring of the imaging stability of the senor and accumulating a large amount of lunar calibration data to establish a lunar radiation model independently in China.

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Keywords

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