光学遥感器小型化对于空间遥感是非常重要的。
The miniaturization of the optical remote sensors is important for the space remote sensing.
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 spectral waveband is an important factor to be investigated in optical remote sensor design.
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 structure scheme of baffle for space optical remote sensor is selected by means of finite element method.
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。
The article analyzes the formulation of the polarization of optical remote sensor and its regulation with the radiant sensitivity of remote sensing system.
文中对德国、法国、印度和美国航天光学遥感器研制情况的一个侧面进行了简述。
The paper introduces the development of space remote sensors in Germany, France, India and America.
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。
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.
TMA空间光学系统可以同时实现大视场和轻型化，在目前空间光学遥感器中得到了广泛的应用。
TMA space optical system can obtain wide field of view and lightweight simultaneously, so this kind of space telescope has been applied widely in the current.
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。
Dynamic environment in launching and thermal environment on orbit affect dimension stability of space optical remote sensor, thus declining its imaging quality.
次镜组件是空间光学遥感器中至关重要的一个组件，次镜组件中的柔性铰链又是次镜组件的一个重要组成部分。
The secondary mirror unit is one of the most important part in the spaceborne remote sensor, and the flexure hinge is a crucial component of the secondary mirror unit.
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.
针对空间光学遥感器反射镜结构刚度高、热尺寸稳定性差的状况，设计了一种柔性锥套结构，它在保持结构刚度满足力学要求的同时，使反射镜具有良好的热尺寸稳定性。
In order to make reflectors of the space remote sensor keep both high rigidity of structure and fine stability of thermal dimension, a kind of flexible cone-shaped sheath is designed.
动力学环境是空间光学遥感器及其组件研制中不可忽视的一个重要因素，因为它会对整机或组件造成结构性的破坏，所以在其研制的不同阶段须进行充分的动力学环境试验。
Dynamics environment is a very important factor for the development of space optics remote sensors because it can bring about damage to the structure of the equipment and its subassemblies.
为了验证该方法的有效性，针对变形较大和传感器位移较大的光学遥感图像设计了仿真实验。
To validate the efficiency of the method, simulation experiments are applied for the optical images with large deformation and with large displacement of the sensor.
概述了当前航天光学成像遥感器在对地、对天观测的多个领域的应用现状及其达到的性能指标。
Recent development status and equipments performance of space optical remote sensors in both earth and space detection fields are described.
概述了当前航天光学成像遥感器在对地、对天观测的多个领域的应用现状及其达到的性能指标。
Recent development status and equipments performance of space optical remote sensors in both earth and space detection fields are described.
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