李响, 白东伟, 孟立新, 高亮, 安岩. 空间碎片探测与测距复合系统光学望远镜[J]. 红外与激光工程, 2021, 50(7): 20200464. DOI: 10.3788/IRLA20200464
引用本文: 李响, 白东伟, 孟立新, 高亮, 安岩. 空间碎片探测与测距复合系统光学望远镜[J]. 红外与激光工程, 2021, 50(7): 20200464. DOI: 10.3788/IRLA20200464
Li Xiang, Bai Dongwei, Meng Lixin, Gao Liang, An Yan. Optical telescope of space debris detection and ranging compound system[J]. Infrared and Laser Engineering, 2021, 50(7): 20200464. DOI: 10.3788/IRLA20200464
Citation: Li Xiang, Bai Dongwei, Meng Lixin, Gao Liang, An Yan. Optical telescope of space debris detection and ranging compound system[J]. Infrared and Laser Engineering, 2021, 50(7): 20200464. DOI: 10.3788/IRLA20200464

空间碎片探测与测距复合系统光学望远镜

Optical telescope of space debris detection and ranging compound system

  • 摘要: 针对空间碎片探测与测距复合系统地面验证演示实验中,工作环境10~30 ℃、光学基台的尺寸限制(不超过450 mm×400 mm)以及光学望远镜尾部安装导致重心远离安装面的问题,提出了空间碎片探测与测距复合系统光学望远镜的设计。使用ANSYS有限元分析软件对光学望远镜建立了有限元模型,针对环境温度10~30 ℃、尾部安装状态下、光轴方向和垂直光轴方向1 gg=9.8 m/s2)重力加速度工况下进行了分析。分析结果表明:光学望远镜整机一阶模态为133 Hz动态刚度较好,重力为光轴方向时主次镜间距最大变化量0.01 mm,重力为垂直光轴方向时主次镜间距最大为0.007 mm,光学望远镜系统波像差RMS值为λ/15,次镜最大倾角1.93″,具有较好的力、热稳定性,可以满足光学天线装校、检测以及外场实验验证过程中的指标要求。在光学望远镜装校完成后,使用ZYGO干涉仪对其像质进行检测,在重力垂直于光轴方向、环境温度10、20、30 ℃条件下进行检测,结果显示:系统波像差RMS值分别为0.097λ、0.075λ及0.1λ,整机光学望远镜系统波像差RMS值在最低温与最高温度时均优于λ/10均满足系统使用要求。

     

    Abstract: In the ground verification demonstration experiment of the space debris detection and ranging composite system, the working environment is 10-30 ℃, the size limit of the optical base station (not exceeding 450 mm×400 mm) and the installation of the tail of the optical telescope cause the center of gravity to be far away from the mounting surface. Design of optical telescope for space debris detection and ranging compound system was proposed. The finite element model of the optical telescope was established by using ANSYS finite element analysis software. The analysis was carried out under the conditions of ambient temperature of 10-30 ℃, tail installation, optical axis direction and vertical optical axis direction of 1 g (g = 9.8 m/s2) gravity acceleration. The analysis results show that the first-order mode of the optical telescope is 133 Hz and the dynamic stiffness is better. When the gravity is in the direction of the optical axis, the maximum change in the distance between the primary and secondary mirrors is 0.01 mm. When the gravity is perpendicular to the optical axis, the maximum distance between the primary and secondary mirrors is 0.007 mm. The RMS value of the wave aberration of the optical telescope system is λ/15, and the maximum inclination angle of the secondary mirror is 1.93″. It has good power and thermal stability and can meet the index requirements in the process of optical antenna installation, calibration, testing and field experiment verification. After the optical telescope is assembled and calibrated, the image quality of the optical telescope is tested using a ZYGO interferometer. The test is performed under the conditions of gravity perpendicular to the optical axis and ambient temperature of 10 ℃, 20 ℃, and 30 ℃. The results show that the RMS value of the system wave phase difference is respectively at 0.097λ, 0.075λ and 0.1λ, the RMS value of the wave phase difference of the whole optical telescope system is better than λ/10 at the lowest temperature and the highest temperature, and all meet the requirements of the system.

     

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