Design of Positioning Mechanism Fit Clearances Based on On-Orbit Re-Orientation Accuracy

The factors affecting the re-orientation accuracy of the on-orbit replaceable optical unit were studied, and the mathematical models of the relationships between fit clearances of positioning mechanisms and the limits of rotation angles were deduced. When the relative position relationship of positi...

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Main Authors: Qingya Li, Libao Yang, Weiguo Zhao, Zhen Shi, Zhenyu Liu
Format: Article
Language:English
Published: MDPI AG 2019-11-01
Series:Applied Sciences
Subjects:
Online Access:https://www.mdpi.com/2076-3417/9/21/4712
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spelling doaj-6f1387e8a3ae46659f771dbdc6ece9fd2020-11-25T01:18:38ZengMDPI AGApplied Sciences2076-34172019-11-01921471210.3390/app9214712app9214712Design of Positioning Mechanism Fit Clearances Based on On-Orbit Re-Orientation AccuracyQingya Li0Libao Yang1Weiguo Zhao2Zhen Shi3Zhenyu Liu4Changchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, ChinaChangchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, ChinaChangchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, ChinaChangchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, ChinaChangchun Institute of Optics, Fine Mechanics and Physics, Chinese Academy of Sciences, Changchun 130033, ChinaThe factors affecting the re-orientation accuracy of the on-orbit replaceable optical unit were studied, and the mathematical models of the relationships between fit clearances of positioning mechanisms and the limits of rotation angles were deduced. When the relative position relationship of positioning mechanisms was determined, fit clearances were designed according to the requirement of the rotation angle limits, and the rotation angle limits were determined to ensure that the angles were within the index range. Theodolites were used to measure the re-orientation angles of the optical unit, and the errors between the measurement angles and the real angles were deduced. Then, the numerical simulation proved that the errors were within limits. The microgravity test environment was established, and the weight of the optical unit was unloaded by a suspension method to simulate the state of the optical unit when it was replaced on orbit. The test results confirmed the correctness of the design method.https://www.mdpi.com/2076-3417/9/21/4712on-orbit replacementoptical unitre-orientation accuracyfit clearances design
collection DOAJ
language English
format Article
sources DOAJ
author Qingya Li
Libao Yang
Weiguo Zhao
Zhen Shi
Zhenyu Liu
spellingShingle Qingya Li
Libao Yang
Weiguo Zhao
Zhen Shi
Zhenyu Liu
Design of Positioning Mechanism Fit Clearances Based on On-Orbit Re-Orientation Accuracy
Applied Sciences
on-orbit replacement
optical unit
re-orientation accuracy
fit clearances design
author_facet Qingya Li
Libao Yang
Weiguo Zhao
Zhen Shi
Zhenyu Liu
author_sort Qingya Li
title Design of Positioning Mechanism Fit Clearances Based on On-Orbit Re-Orientation Accuracy
title_short Design of Positioning Mechanism Fit Clearances Based on On-Orbit Re-Orientation Accuracy
title_full Design of Positioning Mechanism Fit Clearances Based on On-Orbit Re-Orientation Accuracy
title_fullStr Design of Positioning Mechanism Fit Clearances Based on On-Orbit Re-Orientation Accuracy
title_full_unstemmed Design of Positioning Mechanism Fit Clearances Based on On-Orbit Re-Orientation Accuracy
title_sort design of positioning mechanism fit clearances based on on-orbit re-orientation accuracy
publisher MDPI AG
series Applied Sciences
issn 2076-3417
publishDate 2019-11-01
description The factors affecting the re-orientation accuracy of the on-orbit replaceable optical unit were studied, and the mathematical models of the relationships between fit clearances of positioning mechanisms and the limits of rotation angles were deduced. When the relative position relationship of positioning mechanisms was determined, fit clearances were designed according to the requirement of the rotation angle limits, and the rotation angle limits were determined to ensure that the angles were within the index range. Theodolites were used to measure the re-orientation angles of the optical unit, and the errors between the measurement angles and the real angles were deduced. Then, the numerical simulation proved that the errors were within limits. The microgravity test environment was established, and the weight of the optical unit was unloaded by a suspension method to simulate the state of the optical unit when it was replaced on orbit. The test results confirmed the correctness of the design method.
topic on-orbit replacement
optical unit
re-orientation accuracy
fit clearances design
url https://www.mdpi.com/2076-3417/9/21/4712
work_keys_str_mv AT qingyali designofpositioningmechanismfitclearancesbasedononorbitreorientationaccuracy
AT libaoyang designofpositioningmechanismfitclearancesbasedononorbitreorientationaccuracy
AT weiguozhao designofpositioningmechanismfitclearancesbasedononorbitreorientationaccuracy
AT zhenshi designofpositioningmechanismfitclearancesbasedononorbitreorientationaccuracy
AT zhenyuliu designofpositioningmechanismfitclearancesbasedononorbitreorientationaccuracy
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