Acquisition of the Flight Information Using the KSR-3 Agnetometer

The KSR-3 magnetometers consist of the fluxgate magnetometer (MAG/AIM) for acquiring the rocket flight attitude information, and the search-coil magnetometer (MAG/SIM) for the observation of the Earth's magnetic fluctuations. The position (latitude, longitude, and height) and flight condition (...

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Main Authors: Sun-Mi Kim, Min-Hwan Jang, Dong-Hun Lee, Young-Seok Han, Jun Kim, Seung-Hyun Hwang, Eun-Seok Lee, Sun-Min Lee, Hyo-Jin Kim, Su Jin Lee
Format: Article
Language:English
Published: The Korean Space Science Society 2003-03-01
Series:Journal of Astronomy and Space Sciences
Subjects:
Online Access:http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2003/v20n1/OJOOBS_2003_v20n1_29.pdf
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author Sun-Mi Kim
Min-Hwan Jang
Dong-Hun Lee
Young-Seok Han
Jun Kim
Seung-Hyun Hwang
Eun-Seok Lee
Sun-Min Lee
Hyo-Jin Kim
Su Jin Lee
author_facet Sun-Mi Kim
Min-Hwan Jang
Dong-Hun Lee
Young-Seok Han
Jun Kim
Seung-Hyun Hwang
Eun-Seok Lee
Sun-Min Lee
Hyo-Jin Kim
Su Jin Lee
author_sort Sun-Mi Kim
collection DOAJ
description The KSR-3 magnetometers consist of the fluxgate magnetometer (MAG/AIM) for acquiring the rocket flight attitude information, and the search-coil magnetometer (MAG/SIM) for the observation of the Earth's magnetic fluctuations. The position (latitude, longitude, and height) and flight condition (the transformation angle) of the rocket is measured after the data based on these two magnetometers are compared with IGRF. The gap in the vector of magnetic field between the position of the launching point and an impact point is taken into account in data reduction. Angular variation of pitch, yaw, and roll can be researched when the data is applied to the coordinate system of the rocket.
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publisher The Korean Space Science Society
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spelling doaj.art-2da90cdd70634f418c22310d3f0bf7062024-02-02T12:53:46ZengThe Korean Space Science SocietyJournal of Astronomy and Space Sciences2093-55872093-14092003-03-01201294210.5140/JASS.2003.20.1.029Acquisition of the Flight Information Using the KSR-3 AgnetometerSun-Mi Kim0Min-Hwan Jang1Dong-Hun Lee2Young-Seok Han3Jun Kim4Seung-Hyun Hwang5Eun-Seok Lee6Sun-Min Lee7Hyo-Jin Kim8Su Jin Lee9Department of Astronomy Space Science, Kyung Hee University 449-701, Korea Department of Astronomy Space Science, Kyung Hee University 449-701, Korea Department of Astronomy Space Science, Kyung Hee University 449-701, Korea Dept. of Computer Science, University of Suwon 445-743, KoreaKorea Aerospace Research Institute (KARI), Yusung, Daejon 305-333, KoreaKorea Aerospace Research Institute (KARI), Yusung, Daejon 305-333, KoreaDepartment of Astronomy Space Science, Kyung Hee University 449-701, Korea Department of Astronomy Space Science, Kyung Hee University 449-701, Korea Mobile Div., MAPiz Co., Ltd., Seoul 151-869, KoreaKorea Aerospace Research Institute (KARI), Yusung, Daejon 305-333, KoreaThe KSR-3 magnetometers consist of the fluxgate magnetometer (MAG/AIM) for acquiring the rocket flight attitude information, and the search-coil magnetometer (MAG/SIM) for the observation of the Earth's magnetic fluctuations. The position (latitude, longitude, and height) and flight condition (the transformation angle) of the rocket is measured after the data based on these two magnetometers are compared with IGRF. The gap in the vector of magnetic field between the position of the launching point and an impact point is taken into account in data reduction. Angular variation of pitch, yaw, and roll can be researched when the data is applied to the coordinate system of the rocket.http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2003/v20n1/OJOOBS_2003_v20n1_29.pdfmagnetometerfluxgateflight attitude
spellingShingle Sun-Mi Kim
Min-Hwan Jang
Dong-Hun Lee
Young-Seok Han
Jun Kim
Seung-Hyun Hwang
Eun-Seok Lee
Sun-Min Lee
Hyo-Jin Kim
Su Jin Lee
Acquisition of the Flight Information Using the KSR-3 Agnetometer
Journal of Astronomy and Space Sciences
magnetometer
fluxgate
flight attitude
title Acquisition of the Flight Information Using the KSR-3 Agnetometer
title_full Acquisition of the Flight Information Using the KSR-3 Agnetometer
title_fullStr Acquisition of the Flight Information Using the KSR-3 Agnetometer
title_full_unstemmed Acquisition of the Flight Information Using the KSR-3 Agnetometer
title_short Acquisition of the Flight Information Using the KSR-3 Agnetometer
title_sort acquisition of the flight information using the ksr 3 agnetometer
topic magnetometer
fluxgate
flight attitude
url http://ocean.kisti.re.kr/downfile/volume/kosss/OJOOBS/2003/v20n1/OJOOBS_2003_v20n1_29.pdf
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