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An adaptive ball-head positioning visual servoing method for aircraft digital assembly

Hua Liu (Department of Mechanical Engineering, Zhejiang University, Hangzhou, China)
Weidong Zhu (Department of Mechanical Engineering, Zhejiang University, Hangzhou, China)
Huiyue Dong (Department of Mechanical Engineering, Zhejiang University, Hangzhou, China)
Yinglin Ke (The State Key Laboratory of Fluid Power Transmission and Control, Zhejiang University, Hangzhou, China and Key Laboratory of Advanced Manufacturing Technology of Zhejiang Province, College of Mechanical Engineering, Zhejiang University, Hangzhou, China)

Assembly Automation

ISSN: 0144-5154

Article publication date: 3 June 2019

Issue publication date: 3 June 2019

336

Abstract

Purpose

To gain accurate support for large aircraft structures by ball joints in aircraft digital assembly, this paper aims to propose a novel approach based on visual servoing such that the positioner’s ball-socket can automatically and adaptively approach the ball-head fixed on the aircraft structures.

Design/methodology/approach

Image moments of circular marker labeled on the ball-head are selected as visual features to control the three translational degrees of freedom (DOFs) of the positioner, where the composite Jacobian matrix is full rank. Kalman–Bucy filter is adopted for its online estimation, which makes the control scheme more flexible without system calibration. A combination of proportional control with sliding mode control is proposed to improve the system stability and compensate uncertainties of the system.

Findings

The ball-socket can accurately and smoothly reach its desired position in a finite time (50 s). Positional deviations between the spherical centers of ball-head and ball-socket in the X-Y plane can be controlled within 0.05 mm which meets the design requirement.

Practical implications

The proposed approach has been integrated into the pose alignment system. It has shown great potential to be widely applied in the leading support for large aircraft structures in aircraft digital assembly.

Originality/value

An adaptive approach for accurate support of large aircraft structures is proposed, which possesses characteristics of high precision, high efficiency and excellent stability.

Keywords

Acknowledgements

National Natural Science Foundation of China: 51575479, 51675479 and 91748204 Special Scientific Research for Civil Aircraft x: MJZ-G-2011-07

Citation

Liu, H., Zhu, W., Dong, H. and Ke, Y. (2019), "An adaptive ball-head positioning visual servoing method for aircraft digital assembly", Assembly Automation, Vol. 39 No. 2, pp. 287-296. https://doi.org/10.1108/AA-05-2018-066

Publisher

:

Emerald Publishing Limited

Copyright © 2019, Emerald Publishing Limited

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