A microprocessor based system for vibration testing of aircraft structures

S. Ganesan
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Abstract

The author describes an instrumentation system for studying the dynamics of aircraft structures and helicopter rotor blade models. The requirements of various systems for microprocessor-based vibration control and analysis of various systems and details of the instrument are presented. The design of a microprocessor system based on DSP (digital signal processing) microprocessors, an interface to various signal sensors, sensor mounting and selection criteria, signal transmission from the rotating structure to a microprocessor input port, signal processing algorithms, multiblade coordinate transformation, and mode shape analyzer implementation details are discussed. The advantages of using multiple DSP microprocessors for this application are given. Advantages such as online display of the result at the testing site, flexibility, and accuracy are highlighted.<>
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基于微处理器的飞机结构振动测试系统
本文介绍了一种用于研究飞机结构和直升机旋翼桨叶模型动力学的仪器系统。介绍了基于微处理器的振动控制的各种系统的要求,并分析了各种系统和仪器的细节。讨论了基于DSP(数字信号处理)微处理器的微处理器系统的设计,各种信号传感器的接口,传感器的安装和选择标准,信号从旋转结构到微处理器输入端口的传输,信号处理算法,多叶片坐标变换,以及模态振型分析仪的实现细节。给出了在此应用中使用多个DSP微处理器的优点。突出了在线显示测试结果、灵活性和准确性等优点。
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