| Accession number;00A0150788 |
| Title;Attitude Determination Using GPS Signals. |
| Author;ISHIJIMA YOSHINORI(Natl. Space Dev. Agency of Jpn.) SUZUKI HIDEHITO(Natl. Space Dev. Agency of Jpn.) MIYANO TOMOYUKI(Natl. Space Dev. Agency of Jpn.) IWAMOTO YOSHIHIRO(Natl. Space Dev. Agency of Jpn.) ITO TOMOO(Toshiba Corp.) |
Journal Title;Proceedings of the Space Sciences and Technology Conference
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Journal Code:S0277A
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ISSN:
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VOL.43rd;NO.;PAGE.195-200(1999)
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| Figure&Table&Reference;FIG.7, TBL.2, REF.3 |
| Pub. Country;Japan |
| Language;Japanese |
| Abstract;Spaceborne GPS navigation technology is recently studied very actively because it is effective to enhance the autonomy of space vehicles on Low Earth Orbit(LEO). Especially, GPS attitude determination technology means that all the states(position, velocity and attitude) of a space vehicle can be estimated only by a GPS receiver, and contributes the simplification of the GN&C sub-system. By using high-performance electronic devices, it becomes much easier to increase the number of receiver channels and to implement an attitude determination software in an on-board processor of a GPS receiver. In this paper, we show the investigation results of GPS attitude determination algorithms and field test results with the functional model of GPS attitude determination. (author abst.) |
