Online Adaptive Method for Obtaining High-Precision Spherical Joint Positions With the Lower Internal Force Assembly of Large-Scale Aircraft Components

被引:0
作者
Li, Yajun [1 ]
Liu, Wei [1 ]
Lu, Hu [2 ]
Gao, Changyong [1 ]
Liu, Runze [1 ]
Chen, Qihang [1 ]
Zhang, Yang [1 ]
机构
[1] Dalian Univ Technol, State Key Lab High Performance Precis Mfg, Dalian 116024, Peoples R China
[2] COMAC Shanghai Aircraft Mfg Co Ltd, Inst Aeronaut Mfg Technol, Shanghai 200120, Peoples R China
基金
中国国家自然科学基金;
关键词
Assembly; Synchronization; Aircraft; Aircraft manufacture; Mathematical models; Accuracy; Calibration; Cables; Vectors; Kinematics; Aircraft assembly; internal force (IF); posture alignment; posture-coupled error; spherical joint; TRACKING CONTROL;
D O I
10.1109/TII.2024.3495764
中图分类号
TP [自动化技术、计算机技术];
学科分类号
0812 ;
摘要
The high-quality assembly of large-scale aircraft components (LACs) is crucial for modern aircraft manufacturing. The spherical joints are important parts connecting the numerical control locators (NCLs) and LAC. Nevertheless, determining the position of spherical joint centers (SJCs) is challenging because more than half of the ball heads are wrapped inside the ball sockets. Furthermore, the multiaxis asynchronous motion of NCLs will cause internal forces during the posture adjustment process, reducing assembly quality. Hence, an online adaptive scheme with lower internal forces is proposed to obtain the high-precision SJC positions. First, an innovative mathematical model for determining SJC positions with a Jacobian matrix is constructed, and a high-precision solution is achieved via the adaptive estimation Jacobian matrix method, transforming problems that cannot be directly measured into computable solutions. Second, a multiaxis synchronization error is introduced and its mapping relationship with posture-coupled error is established to ensure coordinated NCL motion and reduce internal forces. Finally, the effectiveness of the proposed method is demonstrated through experiments. The maximum error for SJC positions is 0.19 mm, a notable improvement from 0.4 mm. By introducing synchronization error, the internal force is decreased by at least 54%, and its fluctuation range by 54.9%, thereby ensuring assembly quality. This study provides a new method for improving aircraft assembly quality.
引用
收藏
页码:2194 / 2203
页数:10
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