Spacecraft Angular Rates Estimation with Gyrowheel Based on Extended High Gain Observer

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چکیده

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Spacecraft Angular Rates Estimation with Gyrowheel Based on Extended High Gain Observer

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ژورنال

عنوان ژورنال: Sensors

سال: 2016

ISSN: 1424-8220

DOI: 10.3390/s16040537