每年出版 12 期
ISSN 打印: 1064-2315
ISSN 在线: 2163-9337
Indexed in
Identifying Failures in Sensors of a Spacecraft Attitude Control System
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摘要
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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