Transactions of the Society of Instrument and Control Engineers
Online ISSN : 1883-8189
Print ISSN : 0453-4654
ISSN-L : 0453-4654
Attitude Estimation Filter For Gyroless Spacecraft
Utility of Fly-Wheel Angular Velocity Measurements
Shigemune TANIWAKIYoshiaki OHKAMI
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2003 Volume 39 Issue 1 Pages 43-50

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Abstract
A real-time attitude estimation filter for the gyroless spacecrafts is proposed. In this method, outputs from a fly-wheel tachmeter is used. Attitude angular velocity is estimated from wheel angular velocity with use of algebraic relation between them based on angular momentum equation. Extended Kalman filter is used for compensation of sensor noises and drift of total angular momentum caused by external disturbances. The estimator's performance is demonstrated via numerical simulations.
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