Li Shiqi, Zhang Heng, Liu Shiping, Wang Yue
School of Mechanical Science and Engineering, Huazhong University of Science and Technology, Wuhan 430074, China.
Beijing Institute of Space Mechanics and Electricity, Beijing 100094, China.
Rev Sci Instrum. 2018 May;89(5):054901. doi: 10.1063/1.5005590.
This paper presents a framework for the multilevel microvibration analysis and test of a space optical load platform. The test framework is conducted on three levels, including instrument, subsystem, and system level. Disturbance source experimental investigations are performed to evaluate the vibration amplitude and study vibration mechanism. Transfer characteristics of space camera are validated by a subsystem test, which allows the calculation of transfer functions from various disturbance sources to optical performance outputs. In order to identify the influence of the source on the spacecraft performance, a system level microvibration measurement test has been performed on the ground. From the time domain analysis and spectrum analysis of multilevel microvibration tests, we concluded that the disturbance source has a significant effect on its installation position. After transmitted through mechanical links, the residual vibration reduces to a background noise level. In addition, the angular microvibration of the platform jitter is mainly concentrated in the rotation of y-axes. This work is applied to a real practical application involving the high resolution satellite camera system.
本文提出了一种用于空间光学载荷平台多级微振动分析与测试的框架。该测试框架在三个层面上进行,包括仪器级、子系统级和系统级。开展干扰源实验研究以评估振动幅度并研究振动机理。通过子系统测试验证空间相机的传递特性,这使得能够计算从各种干扰源到光学性能输出的传递函数。为了确定该源对航天器性能的影响,已在地面上进行了系统级微振动测量测试。从多级微振动测试的时域分析和频谱分析中,我们得出结论,干扰源对其安装位置有显著影响。通过机械链路传输后,残余振动降低到背景噪声水平。此外,平台抖动的角微振动主要集中在y轴的旋转上。这项工作应用于涉及高分辨率卫星相机系统的实际应用中。