space optical remote sensor 空间光学遥感仪器
The structure scheme of baffle for space optical remote sensor is selected by means of finite element method.
利用有限元工程分析技术对空间光学遥感器的遮光罩结构方案进行了选择。
Dynamic environment in launching and thermal environment on orbit affect dimension stability of space optical remote sensor, thus declining its imaging quality.
发射过程中的力学环境和在轨运行时的热环境，影响航天光学遥感器的尺寸稳定性，进而影响成像质量。
The cylindrical electronic control box for the space optical remote sensor could work normally in the complex environment of space, meet the operation requirements.
设计的空间相机圆柱形电控箱能在复杂的空间环境下正常工作，满足航天使用要求。
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