As an example of large sized structural component, the mechanical model of load calibrationtest of an airplane wing was analysed.
以飞机机翼等大型结构为例,探讨了大型结构部件载荷标定试验的力学模型。
2
Based on the calibrationtest, the model parameters are determined, and the output Angle function can be gotten.
通过标定试验,确定了模型参数,获得了可用于姿态输出的角度计算公式。
3
Introduced are its construction, performance, measurement and control system, automatic data acquisition and processing system, test results of calibrationmodel and analysis, features and USES.