Abstract
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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Li, X., Xu, F., Xu, G. (2023). Redundant IMU Reconfiguration. In: Redundant Inertial Measurement Unit Reconfiguration and Trajectory Replanning of Launch Vehicle. Navigation: Science and Technology, vol 12. Springer, Singapore. https://doi.org/10.1007/978-981-19-4637-0_5
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DOI: https://doi.org/10.1007/978-981-19-4637-0_5
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Publisher Name: Springer, Singapore
Print ISBN: 978-981-19-4636-3
Online ISBN: 978-981-19-4637-0
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