The spectral waveband is an important factor to be investigated in optical remote sensor design.
光谱波段是光学遥感器设计中需要考虑的一个重要指标。
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。
The article analyzes the formulation of the polarization of optical remote sensor and its regulation with the radiant sensitivity of remote sensing system.
文章首先分析了光学遥感器偏振特性的表述及与遥感器系统辐射灵敏度的关系。
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。
The space optical remote sensor is influenced by the solar radiation, albedo, earth emitted infrared and other heat sources as flying in the heat dreariness astrospace.
空间光学遥感器在轨运行过程中要承受太阳辐射和空间冷热沉、黑热沉等恶劣温度环境的影响。
If the capability of MTFC was applied to the design trade-off of optical remote sensor, the developing difficulties could be eased, costs be saved and developing cycles be shortened.
如果综合应用地面MTFC的能力，对遥感器进行优化设计，则可以大大减轻遥感器的研制难度、节约成本和缩短研制周期。
With the development of the space optical remote sensor resolution and the primary mirror diameter, the lightweight design is becoming the key technology of the large aperture mirror.
空间光学遥感器分辨率要求的不断提高使其主镜口径也在不断增大，从而对主镜进行轻量化设计就成为空间大口径反射镜工程的关键技术。
With the development of the space optical remote sensor resolution and the primary mirror diameter, the lightweight design is becoming the key technology of the large aperture mirror.
空间光学遥感器分辨率要求的不断提高使其主镜口径也在不断增大，从而对主镜进行轻量化设计就成为空间大口径反射镜工程的关键技术。
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