摘要
为研究羽流对航天器的影响,需要利用星载可见光探测器实现对可见光谱段的在轨实时监测。其中,关键在于星载可见光探测器的光学性能和力学特性。本文在数字仿真的基础上,通过对光学系统的透过率、光路、温度、成像质量等要素开展光学设计与分析仿真,并通过有限元力学模型开展模态与振动分析,对星载可见光探测器的光学性能和力学性能开展评估,验证了设计合理性。
In order to study the influence of plumes on a spacecraft, it is necessary to use space-borne visible light detectors to realize inorbit real-time monitoring of visible spectrum segments. The key point lies in the optical properties and mechanical properties of space borne visible light detector. In this paper, on the basis of digital simulation, through designing and analysis and simulation of elements such as the transmittance, light path, temperature, the imaging quality of the optical system, and through the finite element method model to conduct modal and vibration analysis, the optical properties and mechanics performance of the space-borne optical detector are evaluated, and the rationality of design is proved.
作者
王俊峰
熊笑
赵晶晶
刘庆海
李昊
王云锋
WANG Jun-Feng;XIONG Xiao;ZHAO Jing-Jing;LIU Qing-Hai;LI Hao;WANG Yun-Feng(Beijing Institute of Spacecraft Environment Engineering,Beijing100094,China;Institute of Spacecraft System Engineering,Beijing100094,China;China Productivity Center for Machinery,Beijing100044,China)
出处
《机电产品开发与创新》
2021年第1期22-25,共4页
Development & Innovation of Machinery & Electrical Products
基金
2018年智能制造综合标准化项目《基于数字仿真的机械产品可靠性测试方法标准研究与试验验证》。
关键词
数字仿真
羽流监测
可见光
有限元
Digital simulation
plumes monitoring
Visible light
FEM