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Attitude determination method using single-antenna GPS, Gyro and Magnetometer

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dc.contributor.authorNo, Heekwon-
dc.contributor.authorHan, Youngmin-
dc.contributor.authorSong, Hongki-
dc.contributor.authorKim, Ojong-
dc.contributor.authorLee, Sungyong-
dc.contributor.authorHan, Deokhwa-
dc.contributor.authorCho, Am-
dc.contributor.authorKee, Changdon-
dc.creator기창돈-
dc.date.accessioned2013-01-25T06:26:15Z-
dc.date.available2013-01-25T06:26:15Z-
dc.date.issued2012-11-13-
dc.identifier.citation2012 Asia-Pacific International Symposium on Aerospace Technology,Nov. 13-15, Jeju, Korea-
dc.identifier.urihttps://hdl.handle.net/10371/81125-
dc.description.abstractIn this paper, we propose the attitude estimation algorithm integrating SAGPS (Single Antenna GPS), Gyroscope and Magnetometer. Pseudo-attitude from SAGPS has low output rate and time delay property. And it differs from actual attitude according to flight condition of airplane because it is based on velocity measurements of GPS. We adopted gyroscope and magnetometer to improve attitude accuracy and output rate of the pseudo-attitude. For validation of the algorithm, simulation is performed and flight data of small UAV is post-processed and compared with commercial AHRS.-
dc.language.isoenen
dc.publisherThe Korean Society for Aeronautical & Space Sciencesen
dc.subject공학en
dc.subjectAttitude-
dc.subjectSAGPS-
dc.subjectMagnetometer-
dc.titleAttitude determination method using single-antenna GPS, Gyro and Magnetometeren
dc.typeConference Paper-
dc.contributor.AlternativeAuthor노희원-
dc.contributor.AlternativeAuthor조암-
dc.contributor.AlternativeAuthor한영민-
dc.contributor.AlternativeAuthor송홍기-
dc.contributor.AlternativeAuthor김오종-
dc.contributor.AlternativeAuthor이선경-
dc.contributor.AlternativeAuthor한덕화-
dc.contributor.AlternativeAuthor기창돈-
dc.description.srndOAIID:oai:osos.snu.ac.kr:snu2012-01/104/0000003405/4-
dc.description.srndSEQ:4-
dc.description.srndPERF_CD:SNU2012-01-
dc.description.srndEVAL_ITEM_CD:104-
dc.description.srndUSER_ID:0000003405-
dc.description.srndADJUST_YN:N-
dc.description.srndEMP_ID:A000360-
dc.description.srndDEPT_CD:446-
dc.description.srndCITE_RATE:0-
dc.description.srndFILENAME:APISAT2012_Paper_HeekwonNo.pdf-
dc.description.srndDEPT_NM:기계항공공학부-
dc.description.srndEMAIL:kee@snu.ac.kr-
dc.description.srndCONFIRM:Y-
dc.identifier.srnd2012-01/104/0000003405/4-
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