CAJ | 학술논문

真实飞机各部件的运动状态总是和理论状态存在差异，所以在飞机型号研制和试验试飞过程中，掌握飞机的实际运动状态是开展后续工作的基础，而由各种仪器测量结果来分析真实运动状态存在着许多困难。以某型号飞机的襟翼转角分析为例，从激光跟踪仪所测得的结果，分别通过圆模拟法和二面角法来分析襟翼在各卡位下的转角。并对两种方法进行详细的介绍和分析，以寻求合理的方法来消除测量误差、制造误差及结构变形对测量结果的影响，供后续工作的开展实施。
진실비궤각부건적운동상태총시화이론상태존재차이，소이재비궤형호연제화시험시비과정중，장악비궤적실제운동상태시개전후속공작적기출，이유각충의기측량결과래분석진실운동상태존재착허다곤난。이모형호비궤적금익전각분석위례，종격광근종의소측득적결과，분별통과원모의법화이면각법래분석금익재각잡위하적전각。병대량충방법진행상세적개소화분석，이심구합리적방법래소제측량오차、제조오차급결구변형대측량결과적영향，공후속공작적개전실시。
There always exists difference in moving conditions between the real parts and the theoretical parts. So in the process of aircraft design and flight tests, itˊs necessary to know the real moving condition of the aircraft parts. But there exists many problems in the analysis of the real moving condition using a variety of instruments. In this article, we will take the flap rotation angle measurement for example, to analyze the rotation angle using cycle simulation method and dihedral angle method with the data collected by laser tracker. We will introduce and ana-lyze these two methods in detail, in order to search reasonable method to eliminate the influence of measure error, manufacture error and structure deformation to the final results, which will be used in the following working.