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- W2034256590 abstract "An initial quaternion estimation method for the attitude determination of a spacecraft using an onboard star sensor is presented. In this method, we use a sequence of the number of stars in the field of view (FOV) of the star sensor as the measurement instead of the direction vector pairs of stars. A new statistical observation model is derived and coupled with the kinematics model of attitude to develop a cost function of the estimated initial quaternion. The attitude acquisition method proposed herein exploits generalized simulated annealing to optimize the cost function and find the initial quaternion. In addition, a virtual sub-FOV and its shuffling procedure for a more accurate estimation are presented. The performance of the proposed method is quantified using an extensive simulation." @default.
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- W2034256590 date "2007-01-01" @default.
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- W2034256590 title "Initial Attitude Determination Using a Single Star Sensor" @default.
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- W2034256590 doi "https://doi.org/10.2322/tjsass.50.27" @default.
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