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  • Yuanqing Xia; Jinhui Zhang; Kunfeng Lu; Ning Zhou
    978-981-13-1373-8
    2019
    Edition 1
    • Uses the sliding mode variable structure control method system to elaborate on single-aircraft and multi-body aircraft attitude setting and attitude control problems
    • Proposes control laws to enhance the performance of spacecraft systems
    • Suggests methods for meeting the many demands on spacecraft systems, such as strong disturbance rejection and high-precision control
    €280 €252
    10% OFF

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