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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Hindawi Limited
2020-01-01
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Series: | Mathematical Problems in Engineering |
Online Access: | http://dx.doi.org/10.1155/2020/4358901 |
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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 |
_version_ |
1715601429280849920 |