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由于科学技术的飞速发展,测量直升机间隙系统的测试仪器也更新得越来越快,而且测验时所使用的分析、采取和处理实验数据工具也越来越先进,这一系列的发展与进步就整体提高了测试直升机操纵系统动态与静态的参考系数的水平,但同时也存在缺陷,如直升机操纵系统间隙测量的实验更新的速度与其它的发展节奏还达不到一致的节奏,绝大部分的实验方法都是按照以前旧的测量实验方法等。
Due to the rapid development of science and technology, the testing instruments for measuring the helicopter clearance system are also updated faster and faster, and the analysis, the tools for taking and processing experimental data are getting more and more advanced during the test, and this series of developments and improvements As a whole, the dynamic and static reference coefficients of helicopter control system are improved, but there are some shortcomings at the same time. For example, the experimental update speed of helicopter control system gap measurement can not reach the same rhythm with other developmental rhythms. Most of the The experimental methods are in accordance with the previous old measurement experiment method.