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タイトルMagnetometer-Only Attitude and Rate Estimates for Spinning Spacecraft
本文(外部サイト)http://hdl.handle.net/2060/20000084154
著者(英)Ottenstein, N.; Challa, M.; Natanson, G.
著者所属(英)Computer Sciences Corp.
発行日2000-05-31
言語eng
内容記述A deterministic algorithm and a Kalman filter for gyroless spacecraft are used independently to estimate the three-axis attitude and rates of rapidly spinning spacecraft using only magnetometer data. In-flight data from the Wide-Field Infrared Explorer (WIRE) during its tumble, and the Fast Auroral Snapshot Explorer (FAST) during its nominal mission mode are used to show that the algorithms can successfully estimate the above in spite of the high rates. Results using simulated data are used to illustrate the importance of accurate and frequent data.
NASA分類Spacecraft Design, Testing and Performance
レポートNOAIAA Paper 2000-4241
権利Copyright, Distribution as joint owner in the copyright
URIhttps://repository.exst.jaxa.jp/dspace/handle/a-is/226968


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