타이틀 |
Orbit Determination of the Orbital Reentry Experiment(OREX) Vehicle by GPS |
저자 |
Masatoshi Harigae, Masaaki MURATA, Toshiaki TSUJII, Hirokimi SHINGU, HIroshi Tomita, Shun-ichi MATSUMOTO |
Keyword |
Global Positioning System; orbit determination; defferential GPS; OREX; Kalman filter |
URL |
http://send.nal.go.jp/send/jpn/dlpdf.php3/naltr01280.pdf?id=NALTR0001280 |
보고서번호 |
NAL TR-1280 |
발행년도 |
1995.11 |
출처 |
NAL (National Aerospace Laboratory of Japan) |
ABSTRACT |
A Japanese first spaceborne GPS receiver,whithin the Orbital Reentry Experiment(OREX) vehicle,was launched by the H-II launch vehicle on February 4,1994.The observed GPS data are analyzed in this report to evalute the accuracy of orbit detrmination by GPS.We examined four techiques for orbit determination;GPS stand-alone navigation,differential GPS navigation,GPS navigation with the precise ephemeris and GPS/IMU hybrid navigation.These results were evaluated by comparson with independent radar |