Titlebook: Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle; Xuefeng Li,Fan Xu,Guoqiang Xu Book 2023 S

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Model of Launch Vehicle Dynamics and Redundant Strapdown IMUs,gle-meter gyro was analyzed. The information reliability model is established in view of common outliers in the information. Finally, the number of reconfigurable units and the minimum included angle are proposed as intuitive reference indicators for evaluating the performance of system after failure.

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Redundant IMU Reconfiguration,It is required for smart rockets that the redundant strapdown IMUs can be self-reconfigured after failure. After one sensor fails, the control system shall be able to select the remaining sensors for redundant reconfiguration through data fusion.

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Xuefeng Li,Fan Xu,Guoqiang XuPresents long-term experiences in launch vehicle control system design from authors.Offers concise and highly pragmatic content.Focuses on the inertial devices and power system‘s reconstruction scheme

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Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle978-981-19-4637-0Series ISSN 2522-0454 Series E-ISSN 2522-0462

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Navigation: Science and Technologyhttp://image.papertrans.cn/r/image/824584.jpg

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https://doi.org/10.1007/978-981-19-4637-0Launch Vehicle; Redundant Inertial Measurement Unit; IMU; Trajectory Replanning; Aerospace Technology

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Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle

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