In order to verify the dynamics characteristic of a space remote sensing camera, spacecraft and camera dynamics coupling test is needed.
为了检验空间遥感相机的动力学特性，需要对相机与飞船进行动力学耦合试验。
According to the characteristic, relationship with input and output, and test principle of certain type airborne coupling component, a design frame of test instrument based on PC104 is presented.
根据某型飞机交联组件功能特点及输入输出关系，研究其测试原理，给出以PC 104架构的测试仪总体设计方案。
According to the characteristic, relationship with input and output, and test principle of certain type airborne coupling component, a design frame of test instrument based on PC104 is presented.
根据某型飞机交联组件功能特点及输入输出关系，研究其测试原理，给出以PC 104架构的测试仪总体设计方案。
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