Preliminary Design of Tracking Mount for Movable SLR

In this paper, we present the result of preliminary design of tracking mount for ARGO-M which is a movable satellite laser ranging (SLR) system developed by Korea Astronomy and Space Science Institute (KASI). The tracking mount consists of a couple of core parts such as driving motors, encoders an...

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Main Authors: Cheol Hoon Park, Young Su Son, Byung In Kim
Format: Article
Language:English
Published: Korean Space Science Society (KSSS) 2010-06-01
Series:Journal of Astronomy and Space Sciences
Subjects:
Online Access:http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2010/v27n2/OJOOBS_2010_v27n2_135.pdf
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spelling doaj-6f08e2c4268e43f3b89d2dbb29a72ac82020-11-25T01:30:36ZengKorean Space Science Society (KSSS)Journal of Astronomy and Space Sciences2093-55872093-14092010-06-0127213514410.5140/JASS.2010.27.2.135Preliminary Design of Tracking Mount for Movable SLRCheol Hoon Park0Young Su Son1Byung In Kim2Korea Institute of Machinery & Materials, Daejeon 305-343, KoreaKorea Institute of Machinery & Materials, Daejeon 305-343, KoreaKorea Institute of Machinery & Materials, Daejeon 305-343, KoreaIn this paper, we present the result of preliminary design of tracking mount for ARGO-M which is a movable satellite laser ranging (SLR) system developed by Korea Astronomy and Space Science Institute (KASI). The tracking mount consists of a couple of core parts such as driving motors, encoders and bearings, and the requirements of each parts are determined on the basis of the technical consideration. 2D and 3D models for tracking mount were preliminarily designed using the selected core parts. In order to evaluate the validity of the preliminarily design, the simulator to test the elevation axis was designed and manufactured. The test to check the tracking performance and system accuracy of the simulator was performed, and it was confirmed that the preliminary design meets the operating specifications. Additionally, it was found that the repetitive errors and hysteresis errors need to be improved by the additional control algorithm.http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2010/v27n2/OJOOBS_2010_v27n2_135.pdfsatellite laser rangingtracking mountpreliminary designsystem accuracy
collection DOAJ
language English
format Article
sources DOAJ
author Cheol Hoon Park
Young Su Son
Byung In Kim
spellingShingle Cheol Hoon Park
Young Su Son
Byung In Kim
Preliminary Design of Tracking Mount for Movable SLR
Journal of Astronomy and Space Sciences
satellite laser ranging
tracking mount
preliminary design
system accuracy
author_facet Cheol Hoon Park
Young Su Son
Byung In Kim
author_sort Cheol Hoon Park
title Preliminary Design of Tracking Mount for Movable SLR
title_short Preliminary Design of Tracking Mount for Movable SLR
title_full Preliminary Design of Tracking Mount for Movable SLR
title_fullStr Preliminary Design of Tracking Mount for Movable SLR
title_full_unstemmed Preliminary Design of Tracking Mount for Movable SLR
title_sort preliminary design of tracking mount for movable slr
publisher Korean Space Science Society (KSSS)
series Journal of Astronomy and Space Sciences
issn 2093-5587
2093-1409
publishDate 2010-06-01
description In this paper, we present the result of preliminary design of tracking mount for ARGO-M which is a movable satellite laser ranging (SLR) system developed by Korea Astronomy and Space Science Institute (KASI). The tracking mount consists of a couple of core parts such as driving motors, encoders and bearings, and the requirements of each parts are determined on the basis of the technical consideration. 2D and 3D models for tracking mount were preliminarily designed using the selected core parts. In order to evaluate the validity of the preliminarily design, the simulator to test the elevation axis was designed and manufactured. The test to check the tracking performance and system accuracy of the simulator was performed, and it was confirmed that the preliminary design meets the operating specifications. Additionally, it was found that the repetitive errors and hysteresis errors need to be improved by the additional control algorithm.
topic satellite laser ranging
tracking mount
preliminary design
system accuracy
url http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2010/v27n2/OJOOBS_2010_v27n2_135.pdf
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AT youngsuson preliminarydesignoftrackingmountformovableslr
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