The Precision Validation of the Precise Baseline Determination for Satellite Formation

The needs for satellite formation flying are gradually increasing to perform the advanced space missions in remote sensing and observation of the space or Earth. Formation flying in low Earth orbit can perform the scientific missions that cannot be realized with a single spacecraft. One of the var...

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Main Authors: Jong-Yeoun Choi, Sang-Jeong Lee
Format: Article
Language:English
Published: Korean Space Science Society (KSSS) 2011-03-01
Series:Journal of Astronomy and Space Sciences
Subjects:
Online Access:http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2011/v28n1/OJOOBS_2011_v28n1_63.pdf
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spelling doaj-54bd8aa92b624509a8c4b81788969b452020-11-25T00:24:04ZengKorean Space Science Society (KSSS)Journal of Astronomy and Space Sciences2093-55872093-14092011-03-01281637010.5140/JASS.2011.28.1.063The Precision Validation of the Precise Baseline Determination for Satellite FormationJong-Yeoun Choi0Sang-Jeong Lee1Satellite Function Test Department, Korea Aerospace Research Institute, Daejeon 305-333, KoreaDepartment of Electronics Engineering, Chung-Nam National University, Daejeon 305-764, KoreaThe needs for satellite formation flying are gradually increasing to perform the advanced space missions in remote sensing and observation of the space or Earth. Formation flying in low Earth orbit can perform the scientific missions that cannot be realized with a single spacecraft. One of the various techniques of satellite formation flying is the determination of the precise baselines between the satellites within the formation, which has to be in company with the precision validation. In this paper, the baseline of Gravity Recovery and Climate Experiment (GRACE) A and B was determined with the real global positioning system (GPS) measurements of GRACE satellites. And baseline precision was validated with the batch and sequential processing methods using K/Ka-band ranging system (KBR) biased range measurements. Because the proposed sequential method validate the baseline precision, removing the KBR bias with the epoch difference instead of its estimation, the validating data (KBR biased range) are independent of the data validated (GPS-baseline) and this method can be applied to the real-time precision validation. The result of sequential precision validation was 1.5~3.0 mm which is similar to the batch precision validation.http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2011/v28n1/OJOOBS_2011_v28n1_63.pdfprecise baseline determinationprecision validationGravity Recovery and Climate ExperimentK/Ka-band ranging system
collection DOAJ
language English
format Article
sources DOAJ
author Jong-Yeoun Choi
Sang-Jeong Lee
spellingShingle Jong-Yeoun Choi
Sang-Jeong Lee
The Precision Validation of the Precise Baseline Determination for Satellite Formation
Journal of Astronomy and Space Sciences
precise baseline determination
precision validation
Gravity Recovery and Climate Experiment
K/Ka-band ranging system
author_facet Jong-Yeoun Choi
Sang-Jeong Lee
author_sort Jong-Yeoun Choi
title The Precision Validation of the Precise Baseline Determination for Satellite Formation
title_short The Precision Validation of the Precise Baseline Determination for Satellite Formation
title_full The Precision Validation of the Precise Baseline Determination for Satellite Formation
title_fullStr The Precision Validation of the Precise Baseline Determination for Satellite Formation
title_full_unstemmed The Precision Validation of the Precise Baseline Determination for Satellite Formation
title_sort precision validation of the precise baseline determination for satellite formation
publisher Korean Space Science Society (KSSS)
series Journal of Astronomy and Space Sciences
issn 2093-5587
2093-1409
publishDate 2011-03-01
description The needs for satellite formation flying are gradually increasing to perform the advanced space missions in remote sensing and observation of the space or Earth. Formation flying in low Earth orbit can perform the scientific missions that cannot be realized with a single spacecraft. One of the various techniques of satellite formation flying is the determination of the precise baselines between the satellites within the formation, which has to be in company with the precision validation. In this paper, the baseline of Gravity Recovery and Climate Experiment (GRACE) A and B was determined with the real global positioning system (GPS) measurements of GRACE satellites. And baseline precision was validated with the batch and sequential processing methods using K/Ka-band ranging system (KBR) biased range measurements. Because the proposed sequential method validate the baseline precision, removing the KBR bias with the epoch difference instead of its estimation, the validating data (KBR biased range) are independent of the data validated (GPS-baseline) and this method can be applied to the real-time precision validation. The result of sequential precision validation was 1.5~3.0 mm which is similar to the batch precision validation.
topic precise baseline determination
precision validation
Gravity Recovery and Climate Experiment
K/Ka-band ranging system
url http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2011/v28n1/OJOOBS_2011_v28n1_63.pdf
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