The three-axis attitude reconstitution scheme for spin stabilized sounding rockets is presented, using star transit pulse information from a single slit all solid state star sensor. The method, based on Kalman filtering and smoothing, gives accuracies in the arcminute range and has been successfully tested on four different missions in the Swedish sounding rocket program.
High-accuracy sounding rocket attitude estimation using star sensor data
Genaue Lageschaetzung von Raketen durch Daten von Sternsensoren
IEEE Transactions on Aerospace and Electronic Systems ; 14 , 6 ; 891-898
1978
8 Seiten, 8 Bilder, 8 Quellen
Article (Journal)
English
RAKETE , FLUGBAHN , FLUGREGELUNG , STERN , BEWEGUNGSGLEICHUNG , KALMAN-FILTER , SENSOR , GENAUIGKEIT , FEHLERSCHAETZUNG
Application of Adaptive Control - Sounding Rocket Attitude
British Library Conference Proceedings | 1997
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