Actuator fault detection method of quadrotor UAV based on dual channel inertial sensors

Laihong Zhou, Hong Jin, Ping Chen, Jianqiang Xiong, Chengdi Li, Wenming Xiong

Open source

DOI: 10.1007/s42452-025-07403-5
Published: 2025-07-02
Container: Discover Applied Sciences
Publisher: Springer Science and Business Media LLC
Open access: unknown

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Cite this work

BibTeX

@article{allodium:10.1007/s42452-025-07403-5,
  title = {Actuator fault detection method of quadrotor UAV based on dual channel inertial sensors},
  author = {Laihong Zhou and Hong Jin and Ping Chen and Jianqiang Xiong and Chengdi Li and Wenming Xiong},
  year = {2025},
  journal = {Discover Applied Sciences},
  doi = {10.1007/s42452-025-07403-5},
  url = {https://doi.org/10.1007/s42452-025-07403-5}
}

RIS

TY  - JOUR
TI  - Actuator fault detection method of quadrotor UAV based on dual channel inertial sensors
AU  - Laihong Zhou
AU  - Hong Jin
AU  - Ping Chen
AU  - Jianqiang Xiong
AU  - Chengdi Li
AU  - Wenming Xiong
PY  - 2025
JO  - Discover Applied Sciences
DO  - 10.1007/s42452-025-07403-5
UR  - https://doi.org/10.1007/s42452-025-07403-5
ER  -

APA

Zhou, L., Jin, H., Chen, P., Xiong, J., Li, C., & Xiong, W. (2025). Actuator fault detection method of quadrotor UAV based on dual channel inertial sensors. Discover Applied Sciences. https://doi.org/10.1007/s42452-025-07403-5

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crossref · retrieved 2026-11-10T09:42:56.879Z