具体提出结构的总体框架设计和动态性能演算数学模型，同时提出控制系统设计思想及相关设计原则。

Then, this thesis puts forward the overall system architecture and the models for the dynamical performance, as well as the ideas and principles in the design of the control system.

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其次结合飞机的曲面外形，建立了飞机结构静力试验设计中的分布式载荷和集中式载荷的演算数学模型。

Then, the mathematics model of calculating the surface load and point load in the design of aircraft structure static load test using aircraft surface model is established.

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