Algorithm for in-flight gyroscope calibration

Details Algorithm for in-flight gyroscope calibration Algorithm for in-flight gyroscope calibration

Sep 1988

adsabs.harvard.edu/cgi-bin/nph-data_query?bibcode=1988fmet.symp..114d&link_type=abstract

In its Flight Mechanics/Estimation Theory Symposium 1988 p 114-127 (SEE N89-15934 08-13)

Physics

Attitude Control, Gyroscopic Stability, Hubble Space Telescope, Accuracy, Algorithms, Calibrating

Scientific paper

An optimal algorithm for the in-flight calibration of spacecraft gyroscope systems is presented. Special consideration is given to the selection of the loss function weight matrix in situations in which the spacecraft attitude sensors provide significantly more accurate information in pitch and yaw than in roll, such as will be the case in the Hubble Space Telescope mission. The results of numerical tests that verify the accuracy of the algorithm are discussed.

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