新一代海洋水色观测卫星水色遥感器光机系统设计与验证

    Opto-mechanical system design and verification for the ocean color remote sensor of the new generation ocean color observation satellite

    • 针对中国“海洋一号”卫星水色遥感器波段数量少、信噪比不足、空间分辨率低、杂散光和偏振灵敏度抑制不够及定标系统精度低等问题,新一代海洋水色遥感器采用先进的望远镜整体旋转光机扫描成像方式。遥感器光学系统采用旋转式离轴三反系统,既消除了光学系统像旋,又有利于杂散光和偏振灵敏度的控制。光机结构采用U形架结构形式,在控制系统质量的同时确保了系统支撑刚度。光机扫描机构采用基于多烷基化环戊烷(multiply-alkylated cyclopentanes,MACs)基的油脂润滑轴承,确保机构的使用寿命达到8年。光机系统的定标装置采用全口径、全光路的背靠背式双漫反射板太阳定标方案,保证了漫反射板的在轨寿命。验证结果表明:该遥感器在CAST2000小卫星平台上实现了覆盖0.35~12.5 μm共18个波段,信噪比≥1 000,空间分辨率≤500 m,偏振灵敏度≤1.5%,杂光系数≤1%的对地成像。经动不平衡补偿后,机构对小卫星平台的姿态扰动小于0.005(°)/s,星上太阳定标精度优于2%。基于这些优点,所提方法特别适用于小卫星平台上的多波段、高定量化遥感器,具有广阔的应用前景。

       

      Abstract: To address the shortcomings of China's HY-1 Satellite ocean color remote sensor, such as limited spectral bands, insufficient signal-to-noise ratio, low spatial resolution, inadequate suppression of stray light and polarization sensitivity, and low-precision calibration system, an overall rotating opto-mechanical scanning imaging approach of the advanced telescope was adopted by the new generation ocean color sensor. A rotating off-axis three-mirror system was employed by the remote sensor optical system, eliminating optical system image rotation while enhancing stray light and polarization sensitivity control. A U-shaped frame design was adopted by the opto-mechanical system, controlling the system weight while ensuring system structural rigidity. A grease-lubricated bearing based on MACs was utilized by the opto-mechanical scanning mechanism, ensuring an 8-year lifespan of the mechanism. A full-aperture, full-light-path, back-to-back dual diffuse reflector solar calibration scheme was employed by the calibration device of the opto-mechanical system, guaranteeing the on-orbit lifespan of the diffuse reflectors. The verification results show that the remote sensor using this proposed approach achieves Earth imaging with 18 spectral bands covering 0.35~12.5 μm, signal-to-noise ratio≥1 000, spatial resolution≤500 m, polarization sensitivity≤1.5%, and stray light coefficient≤1% on the CAST2000 small satellite platform. The attitude disturbance of the mechanism to the small satellite platform is less than 0.005(°)/s after dynamic imbalance compensation. The on-board solar calibration accuracy is better than 2%. Because of these advantages, the proposed approach is particularly suitable for multi-band, high-quantification remote sensors on small satellite platforms with promising application prospects.

       

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