建立了陀螺的高过载设计约束条件，包括陀螺所选用类型与尺寸参数。
The restriction of gyroscope's high overloading are presented, including gyroscope's style and structure dimension.
最后从杂波自由度得到分布式小卫星雷达实现地面运动目标指示的基本设计约束条件。
Basic design constraints of the distributed small satellite based GMTI radar are derived from the clutter rank.
围绕主镜的设计约束条件，本文主要介绍了主镜材料的选择和几个典型结构参数的确定。
Around design requirements of the primary mirror, the article mainly introduces the process of the primary mirror material selection and some structure parameter's decision.
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