摘要
提出了飞机大部件自动对接同步调姿方法,实现了大部件调姿基准点的连续自动跟踪测量和位姿连续调整。在此基础上开发了集测量场构建、大部件位姿解算和调整等功能于一体的大部件自动对接集成控制软件,并在ARJ21飞机翼身自动对接现场进行了应用试验,结果证明该方法能有效完成飞机翼身自动对接过程,提高测量和对接效率。
A synchronous position and pose adjustment method for large aircraft components＇ automatic assembly is proposed, of which the continuous automatic tracking measurement of reference points and continuous position and pose adjustment of large aircraft components are realized. On this basis, an integrated control software is developed, which integrates functions such as the construction of measurement field, the position and pose calculation and adjustment of large aircraft components. An application experiment has been done on the automatic assembly of fuselage and wings of ARJ21 airplane, which demonstrated that the method can complete the assembly process effectively and improve the efficiency of measurement and assembly.
出处
《航空制造技术》
2016年第4期52-56,共5页
Aeronautical Manufacturing Technology
基金
国家自然科学基金资助项目(51275234)
航空科学基金资助项目(20132252027)
关键词
大部件自动对接
同步调姿
连续自动跟踪测量
Automatic assembly of large aircraft components
Synchronous position and pose adjustment
Continuous automatic tracking measurement
