摘要
针对直升机动力学试验中载荷难于准确测量且各分量间耦合大的难题,研制了一种新型结构的八维六自由度动态测力装置。介绍了八维六自由度动态测力装置的结构设计原理、测量算法、标定及在直升机动力学试验中的应用情况。
It was hard to accurately measure the load in helicopter dynamics test and the distribution coupling is big.So the writer developed this new 8 dimensional space six degrees of freedom force-measuring device.This paper introduced the structure,measuring method,calibration and it was application in helicopter dynamics test.
出处
《直升机技术》
2010年第3期62-67,共6页
Helicopter Technique
关键词
动态测力装置
八维六自由度
动力学试验
force-measuring device
eight-dimensional space six degrees of freedom
dynamics test
