Выходит 12 номеров в год
ISSN Печать: 1064-2315
ISSN Онлайн: 2163-9337
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Identifying Failures in Sensors of a Spacecraft Attitude Control System
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Краткое описание
A problem of failure detection and identification in sensors of a spacecraft attitude control system under condition of their minimum number or minimum redundancy is investigated. The effectiveness of procedures under consideration is illustrated via angular rate sensors and Sun sensor as examples.
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Lysenko L.N., Aiming and navigation of ballistic rockets.
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Potter J.E., Deckert J.C., Minimax failure detection and identification in redundant gyro and accelerometer systems.
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Wilcox J.C., Competitive evaluation of failure detection algorithms for strapdown inertial instruments.
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Deyst J.J., Harrison J.V., Gai E., Daly K.C., Fault detection, identification and reconfiguration for spacecraft systems.
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Frank P.M., Fault diagnosis in dynamic systems using analytical and knowledge-based redundancy – a survey and some new results.
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Lebedev D.V., Identification of failures in a unit of sensing elements of inertial navigation system.
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Gantmakher F.R., Matrix theory.
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Chow E.Y., Willsky A.S., Analytical redundancy and the design of robust failure detection systems.
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Lou X.-C., Willsky A.S., Verghese G.C., Optimally robust redundancy relations for failure detection in uncertain systems.
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Lebedev D.V., Tkachenko A.I., Information-algorithmic aspects of mobile object control.
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Lebedev D.V., Tkachenko A.I., Navigation and control of attitude of small spacecrafts.