Accuracy Improvement Calibrations for the Double-Position 4-PPPS Aircraft Docking System

A double-positions 4-PPPS parallel mechanism is used for the aircraft fuselage assembly process to improve the docking efficiency and reduce the labor intensity. However, the accuracy is hard to guarantee, for the mechanism is large and redundant and has manufacturing and assembly errors. To improve...

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Main Authors: Ruolong Qi, Yuangui Tang, Ke Zhang
Format: Article
Language:English
Published: Hindawi Limited 2020-01-01
Series:Mathematical Problems in Engineering
Online Access:http://dx.doi.org/10.1155/2020/4358901
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spelling doaj-06203990da43447bafef73d96ef359a72020-11-25T02:00:30ZengHindawi LimitedMathematical Problems in Engineering1024-123X1563-51472020-01-01202010.1155/2020/43589014358901Accuracy Improvement Calibrations for the Double-Position 4-PPPS Aircraft Docking SystemRuolong Qi0Yuangui Tang1Ke Zhang2School of Mechanical Engineering, Shenyang Jianzhu University, Shenyang, Liaoning, ChinaThe State Key Laboratory of Robotics, Shenyang Institute of Automation, Chinese Academy of Sciences, Shenyang, Liaoning, ChinaSchool of Mechanical Engineering, Shenyang Jianzhu University, Shenyang, Liaoning, ChinaA double-positions 4-PPPS parallel mechanism is used for the aircraft fuselage assembly process to improve the docking efficiency and reduce the labor intensity. However, the accuracy is hard to guarantee, for the mechanism is large and redundant and has manufacturing and assembly errors. To improve the accuracy of the 4-PPPS parallel aircraft fuselage docking system, firstly, an averaging iteration method is proposed to calibrate the datum points in the airplane coordinate which are the references of the entire docking system. And secondly, a kinematic calibration method based on the derivative of the spatial pose transformation is proposed to calibrate up to 42 kinematic parameters. By these two methods, the final maximum position error reduced from 2.2 mm to 0.035 mm and the maximum pointing error reduced from 0.08 degree to 0.018 degree. The accuracy measurement and docking experiment prove the efficiency of the proposed methods.http://dx.doi.org/10.1155/2020/4358901
collection DOAJ
language English
format Article
sources DOAJ
author Ruolong Qi
Yuangui Tang
Ke Zhang
spellingShingle Ruolong Qi
Yuangui Tang
Ke Zhang
Accuracy Improvement Calibrations for the Double-Position 4-PPPS Aircraft Docking System
Mathematical Problems in Engineering
author_facet Ruolong Qi
Yuangui Tang
Ke Zhang
author_sort Ruolong Qi
title Accuracy Improvement Calibrations for the Double-Position 4-PPPS Aircraft Docking System
title_short Accuracy Improvement Calibrations for the Double-Position 4-PPPS Aircraft Docking System
title_full Accuracy Improvement Calibrations for the Double-Position 4-PPPS Aircraft Docking System
title_fullStr Accuracy Improvement Calibrations for the Double-Position 4-PPPS Aircraft Docking System
title_full_unstemmed Accuracy Improvement Calibrations for the Double-Position 4-PPPS Aircraft Docking System
title_sort accuracy improvement calibrations for the double-position 4-ppps aircraft docking system
publisher Hindawi Limited
series Mathematical Problems in Engineering
issn 1024-123X
1563-5147
publishDate 2020-01-01
description A double-positions 4-PPPS parallel mechanism is used for the aircraft fuselage assembly process to improve the docking efficiency and reduce the labor intensity. However, the accuracy is hard to guarantee, for the mechanism is large and redundant and has manufacturing and assembly errors. To improve the accuracy of the 4-PPPS parallel aircraft fuselage docking system, firstly, an averaging iteration method is proposed to calibrate the datum points in the airplane coordinate which are the references of the entire docking system. And secondly, a kinematic calibration method based on the derivative of the spatial pose transformation is proposed to calibrate up to 42 kinematic parameters. By these two methods, the final maximum position error reduced from 2.2 mm to 0.035 mm and the maximum pointing error reduced from 0.08 degree to 0.018 degree. The accuracy measurement and docking experiment prove the efficiency of the proposed methods.
url http://dx.doi.org/10.1155/2020/4358901
work_keys_str_mv AT ruolongqi accuracyimprovementcalibrationsforthedoubleposition4pppsaircraftdockingsystem
AT yuanguitang accuracyimprovementcalibrationsforthedoubleposition4pppsaircraftdockingsystem
AT kezhang accuracyimprovementcalibrationsforthedoubleposition4pppsaircraftdockingsystem
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