Performance Analysis of Ranging Techniques for the KPLO Mission

In this study, the performance of ranging techniques for the Korea Pathfinder Lunar Orbiter (KPLO) space communication system is investigated. KPLO is the first lunar mission of Korea, and pseudo-noise (PN) ranging will be used to support the mission along with sequential ranging. We compared the pe...
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Autor*in:	Sungjoon Park [verfasserIn] Sangman Moon [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2018

Schlagwörter:	PN ranging sequential ranging accuracy acquisition probability integration time

Übergeordnetes Werk:	In: Journal of Astronomy and Space Sciences - Korean Space Science Society (KSSS), 2012, 35(2018), 1, Seite 39-46
Übergeordnetes Werk:	volume:35 ; year:2018 ; number:1 ; pages:39-46

Links:	Link aufrufen Link aufrufen Link aufrufen Journal toc Journal toc

DOI / URN:	10.5140/JASS.2017.35.1.39

Katalog-ID:	DOAJ007732562

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spelling	10.5140/JASS.2017.35.1.39 doi (DE-627)DOAJ007732562 (DE-599)DOAJ727e5d5d6c614bc7a71ca9b42042edec DE-627 ger DE-627 rakwb eng QB1-991 Sungjoon Park verfasserin aut Performance Analysis of Ranging Techniques for the KPLO Mission 2018 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In this study, the performance of ranging techniques for the Korea Pathfinder Lunar Orbiter (KPLO) space communication system is investigated. KPLO is the first lunar mission of Korea, and pseudo-noise (PN) ranging will be used to support the mission along with sequential ranging. We compared the performance of both ranging techniques using the criteria of accuracy, acquisition probability, and measurement time. First, we investigated the end-to-end accuracy error of a ranging technique incorporating all sources of errors such as from ground stations and the spacecraft communication system. This study demonstrates that increasing the clock frequency of the ranging system is not required when the dominant factor of accuracy error is independent of the thermal noise of the ranging technique being used in the system. Based on the understanding of ranging accuracy, the measurement time of PN and sequential ranging are further investigated and compared, while both techniques satisfied the accuracy and acquisition requirements. We demonstrated that PN ranging performed better than sequential ranging in the signal-to-noise ratio (SNR) regime where KPLO will be operating, and we found that the T2B (weighted-voting balanced Tausworthe, voting v PN ranging sequential ranging accuracy acquisition probability integration time Astronomy Sangman Moon verfasserin aut In Journal of Astronomy and Space Sciences Korean Space Science Society (KSSS), 2012 35(2018), 1, Seite 39-46 (DE-627)62761471X (DE-600)2557343-3 20931409 nnns volume:35 year:2018 number:1 pages:39-46 https://doi.org/10.5140/JASS.2017.35.1.39 kostenfrei https://doaj.org/article/727e5d5d6c614bc7a71ca9b42042edec kostenfrei http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2018/v35n1/OJOOBS_2018_v35n1_39.pdf kostenfrei https://doaj.org/toc/2093-5587 Journal toc kostenfrei https://doaj.org/toc/2093-1409 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 35 2018 1 39-46
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allfieldsSound	10.5140/JASS.2017.35.1.39 doi (DE-627)DOAJ007732562 (DE-599)DOAJ727e5d5d6c614bc7a71ca9b42042edec DE-627 ger DE-627 rakwb eng QB1-991 Sungjoon Park verfasserin aut Performance Analysis of Ranging Techniques for the KPLO Mission 2018 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier In this study, the performance of ranging techniques for the Korea Pathfinder Lunar Orbiter (KPLO) space communication system is investigated. KPLO is the first lunar mission of Korea, and pseudo-noise (PN) ranging will be used to support the mission along with sequential ranging. We compared the performance of both ranging techniques using the criteria of accuracy, acquisition probability, and measurement time. First, we investigated the end-to-end accuracy error of a ranging technique incorporating all sources of errors such as from ground stations and the spacecraft communication system. This study demonstrates that increasing the clock frequency of the ranging system is not required when the dominant factor of accuracy error is independent of the thermal noise of the ranging technique being used in the system. Based on the understanding of ranging accuracy, the measurement time of PN and sequential ranging are further investigated and compared, while both techniques satisfied the accuracy and acquisition requirements. We demonstrated that PN ranging performed better than sequential ranging in the signal-to-noise ratio (SNR) regime where KPLO will be operating, and we found that the T2B (weighted-voting balanced Tausworthe, voting v PN ranging sequential ranging accuracy acquisition probability integration time Astronomy Sangman Moon verfasserin aut In Journal of Astronomy and Space Sciences Korean Space Science Society (KSSS), 2012 35(2018), 1, Seite 39-46 (DE-627)62761471X (DE-600)2557343-3 20931409 nnns volume:35 year:2018 number:1 pages:39-46 https://doi.org/10.5140/JASS.2017.35.1.39 kostenfrei https://doaj.org/article/727e5d5d6c614bc7a71ca9b42042edec kostenfrei http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2018/v35n1/OJOOBS_2018_v35n1_39.pdf kostenfrei https://doaj.org/toc/2093-5587 Journal toc kostenfrei https://doaj.org/toc/2093-1409 Journal toc kostenfrei GBV_USEFLAG_A SYSFLAG_A GBV_DOAJ SSG-OLC-PHA GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_95 GBV_ILN_105 GBV_ILN_110 GBV_ILN_151 GBV_ILN_161 GBV_ILN_170 GBV_ILN_213 GBV_ILN_230 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_2014 GBV_ILN_4012 GBV_ILN_4037 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4249 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4367 GBV_ILN_4700 AR 35 2018 1 39-46
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callnumber-first	Q - Science
author	Sungjoon Park
spellingShingle	Sungjoon Park misc QB1-991 misc PN ranging misc sequential ranging misc accuracy misc acquisition probability misc integration time misc Astronomy Performance Analysis of Ranging Techniques for the KPLO Mission
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topic_title	QB1-991 Performance Analysis of Ranging Techniques for the KPLO Mission PN ranging sequential ranging accuracy acquisition probability integration time
topic	misc QB1-991 misc PN ranging misc sequential ranging misc accuracy misc acquisition probability misc integration time misc Astronomy
topic_unstemmed	misc QB1-991 misc PN ranging misc sequential ranging misc accuracy misc acquisition probability misc integration time misc Astronomy
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title	Performance Analysis of Ranging Techniques for the KPLO Mission
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title_full	Performance Analysis of Ranging Techniques for the KPLO Mission
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title_sort	performance analysis of ranging techniques for the kplo mission
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title_auth	Performance Analysis of Ranging Techniques for the KPLO Mission
abstract	In this study, the performance of ranging techniques for the Korea Pathfinder Lunar Orbiter (KPLO) space communication system is investigated. KPLO is the first lunar mission of Korea, and pseudo-noise (PN) ranging will be used to support the mission along with sequential ranging. We compared the performance of both ranging techniques using the criteria of accuracy, acquisition probability, and measurement time. First, we investigated the end-to-end accuracy error of a ranging technique incorporating all sources of errors such as from ground stations and the spacecraft communication system. This study demonstrates that increasing the clock frequency of the ranging system is not required when the dominant factor of accuracy error is independent of the thermal noise of the ranging technique being used in the system. Based on the understanding of ranging accuracy, the measurement time of PN and sequential ranging are further investigated and compared, while both techniques satisfied the accuracy and acquisition requirements. We demonstrated that PN ranging performed better than sequential ranging in the signal-to-noise ratio (SNR) regime where KPLO will be operating, and we found that the T2B (weighted-voting balanced Tausworthe, voting v
abstractGer	In this study, the performance of ranging techniques for the Korea Pathfinder Lunar Orbiter (KPLO) space communication system is investigated. KPLO is the first lunar mission of Korea, and pseudo-noise (PN) ranging will be used to support the mission along with sequential ranging. We compared the performance of both ranging techniques using the criteria of accuracy, acquisition probability, and measurement time. First, we investigated the end-to-end accuracy error of a ranging technique incorporating all sources of errors such as from ground stations and the spacecraft communication system. This study demonstrates that increasing the clock frequency of the ranging system is not required when the dominant factor of accuracy error is independent of the thermal noise of the ranging technique being used in the system. Based on the understanding of ranging accuracy, the measurement time of PN and sequential ranging are further investigated and compared, while both techniques satisfied the accuracy and acquisition requirements. We demonstrated that PN ranging performed better than sequential ranging in the signal-to-noise ratio (SNR) regime where KPLO will be operating, and we found that the T2B (weighted-voting balanced Tausworthe, voting v
abstract_unstemmed	In this study, the performance of ranging techniques for the Korea Pathfinder Lunar Orbiter (KPLO) space communication system is investigated. KPLO is the first lunar mission of Korea, and pseudo-noise (PN) ranging will be used to support the mission along with sequential ranging. We compared the performance of both ranging techniques using the criteria of accuracy, acquisition probability, and measurement time. First, we investigated the end-to-end accuracy error of a ranging technique incorporating all sources of errors such as from ground stations and the spacecraft communication system. This study demonstrates that increasing the clock frequency of the ranging system is not required when the dominant factor of accuracy error is independent of the thermal noise of the ranging technique being used in the system. Based on the understanding of ranging accuracy, the measurement time of PN and sequential ranging are further investigated and compared, while both techniques satisfied the accuracy and acquisition requirements. We demonstrated that PN ranging performed better than sequential ranging in the signal-to-noise ratio (SNR) regime where KPLO will be operating, and we found that the T2B (weighted-voting balanced Tausworthe, voting v
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title_short	Performance Analysis of Ranging Techniques for the KPLO Mission
url	https://doi.org/10.5140/JASS.2017.35.1.39 https://doaj.org/article/727e5d5d6c614bc7a71ca9b42042edec http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2018/v35n1/OJOOBS_2018_v35n1_39.pdf https://doaj.org/toc/2093-5587 https://doaj.org/toc/2093-1409
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Performance Analysis of Ranging Techniques for the KPLO Mission

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