检索规则说明:AND代表“并且”;OR代表“或者”;NOT代表“不包含”;(注意必须大写,运算符两边需空一格)
检 索 范 例 :范例一: (K=图书馆学 OR K=情报学) AND A=范并思 范例二:J=计算机应用与软件 AND (U=C++ OR U=Basic) NOT M=Visual
作 者:苑泽冰 乐洪博 王福毅 李登辉 YUAN Zebing;LE Hongbo;WANG Fuyi;LI Denghui(Shenyang Aircraft Corporation,Shenyang,Liaoning 110034,China;School of Mechanical and Electronical Engineering,Shenyang Aerospace University,Shenyang,Liaoning 110136,China)
机构地区:[1]沈阳飞机工业(集团)有限公司,辽宁沈阳110034 [2]沈阳航空航天大学机电工程学院,辽宁沈阳110136
出 处:《自动化应用》2024年第13期183-185,共3页Automation Application
摘 要:飞机装配部件具有尺寸较大且形状复杂的特点,装配后的尺寸与理论模型存在偏差,且飞机型面的测量数据量庞大,因此设计一种高效且准确的飞机外形测量方法对保证飞机装配精度至关重要。建立了激光跟踪仪与激光雷达组合的测量系统,用于完成对整机外形的测量任务。该系统包含空间系统定位、坐标系建立、站位划分以及点云密度分布方面的详细方案设计。通过对测量数据与理论模型进行对比和误差分析,验证了综合测量精度符合系统标称场控精度,进而验证了所提方法的可行性和正确性。Aircraft assembly parts are characterized by large size and complex shape,the deviation of the assembled dimensions from the theoretical model,and the huge amount of measurement data of the aircraft profile,so designing an efficient and accurate measurement method of the aircraft profile is crucial to ensure the accuracy of the aircraft assembly.A measurement system combining laser tracker and lidar is established to fulfill the measurement task of the whole aircraft profile.The system includes the detailed program design in terms of spatial system positioning,coordinate system establishment,stations division and point cloud density distribution.By comparing the measurement data with the theoretical model and analyzing the errors,it is verified that the integrated measurement accuracy conforms to the nominal field control accuracy of the system,which in turn verifies the feasibility and correctness of the proposed method.
分 类 号:V262[航空宇航科学与技术—航空宇航制造工程] TN958.98[电子电信—信号与信息处理]
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在载入数据...
正在链接到云南高校图书馆文献保障联盟下载...
云南高校图书馆联盟文献共享服务平台 版权所有©
您的IP:3.145.17.123