Abstract
A hierarchical fault-tolerant controller for a hexacopter is proposed. The proposed control scheme switches from a nominal controller to a fault-tolerant controller when a fault occurs. In the normal operation condition, an adaptive sliding mode controller is used to adjust the control gains that can deal with uncertainties such as disturbance. When failure occurs, the sliding mode controller with control allocation is activated, which uses constant control gain from the previous adaptive sliding mode controller. The effectiveness and robustness of the proposed controller are demonstrated by numerical simulation subject to an actuator failure. Comparison with a conventional adaptive sliding mode control allocation scheme is also shown.
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Acknowledgement
This research was supported by Unmanned Vehicles Core Technology Research and Development Program through the National Research Foundation of Korea (NRF) and Unmanned Vehicle Advanced Research Center (UVARC) funded by the Ministry of Science and ICT, the Republic of Korea (2020M3C1C1A01083162).
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Kim, M., Lee, H., Kim, J., Kim, Sh., Kim, Y. (2022). Hierarchical Fault Tolerant Control of a Hexacopter UAV Against Actuator Failure. In: Kim, J., et al. Robot Intelligence Technology and Applications 6. RiTA 2021. Lecture Notes in Networks and Systems, vol 429. Springer, Cham. https://doi.org/10.1007/978-3-030-97672-9_8
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DOI: https://doi.org/10.1007/978-3-030-97672-9_8
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