榨取
发表于 2025-3-23 10:12:52
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.
GRATE
发表于 2025-3-23 16:33:41
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MAIM
发表于 2025-3-23 21:21:57
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.
五行打油诗
发表于 2025-3-24 00:27:40
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
condone
发表于 2025-3-24 05:42:45
Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle978-981-19-4637-0Series ISSN 2522-0454 Series E-ISSN 2522-0462
物种起源
发表于 2025-3-24 09:12:50
Navigation: Science and Technologyhttp://image.papertrans.cn/r/image/824584.jpg
ellagic-acid
发表于 2025-3-24 13:06:12
https://doi.org/10.1007/978-981-19-4637-0Launch Vehicle; Redundant Inertial Measurement Unit; IMU; Trajectory Replanning; Aerospace Technology
ostracize
发表于 2025-3-24 16:53:52
Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle
钢盔
发表于 2025-3-24 19:09:00
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哀求
发表于 2025-3-25 02:16:44
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