Institute of Optics and Electronics, Chinese Academy of Sciences, Chengdu 610209, China.
Sensors (Basel). 2023 May 17;23(10):4833. doi: 10.3390/s23104833.
The aperture of space telescopes increases with their required resolution, and the transmission optical systems with long focal length and diffractive primary lens are becoming increasingly popular. In space, the changes in the pose of the primary lens relative to the rear lens group have a significant impact on the imaging performance of the telescope system. The measurement of the pose of the primary lens in real-time and with high-precision is one of the important techniques for a space telescope. In this paper, a high-precision real-time pose measurement method for the primary lens of a space telescope in orbit based on laser ranging is proposed, and a verification system is established. The pose change of the telescope's primary lens can be easily calculated through six high-precision laser distance changes. The measurement system can be installed freely, which solves the problems of complex system structure and low measurement accuracy in traditional pose measurement techniques. Analysis and experiments show that this method can accurately obtain the pose of the primary lens in real-time. The rotation error of the measurement system is 2 × 10 degrees (0.072 arcsecs), and the translation error is 0.2 μm. This study will provide a scientific basis for high-quality imaging of a space telescope.
空间望远镜的孔径随其所需分辨率的增加而增大,而具有长焦距和衍射主透镜的透射光学系统越来越受欢迎。在太空中,主透镜相对于后透镜组的姿态变化对望远镜系统的成像性能有重大影响。实时、高精度地测量主透镜的姿态是空间望远镜的重要技术之一。本文提出了一种基于激光测距的在轨空间望远镜主镜高精度实时姿态测量方法,并建立了验证系统。通过六个高精度激光距离变化,很容易计算出望远镜主镜的姿态变化。测量系统可自由安装,解决了传统姿态测量技术中系统结构复杂、测量精度低的问题。分析和实验表明,该方法可以实时、精确地获取主镜的姿态。测量系统的旋转误差为 2×10 度(0.072 弧秒),平移误差为 0.2μm。本研究将为空间望远镜的高质量成像提供科学依据。