Multicopter Fault Detection and Identification via Data-Driven Statistical Learning Methods

This paper presents the introduction, investigation, and critical assessment of three data-driven methods for rotor failure detection and identification in a multicopter. These methods are based on aircraft attitude signals obtained from forward flight under turbulence and uncertainty. The knowledge-based method exploits the system rigid-body dynamics insight under the different rotor failures to construct a decision tree that detects and identifies the rotor failure simultaneously by how the roll, pitch, and yaw signals violate the statistical confidence limits immediately after failure. For the statistical time-series method, the development of stochastic time-series models and residual-based statistical hypothesis tests are discussed. Here, fault detection in the transient response is followed by identification after the signals reach a stationary state, after controller compensation, with the healthy and the different faulty models, respectively, in a two-step manner. The third method employs the healthy time-series model to extract a useful feature, which is the residual cross correlation, as an input to a neural network trained to achieve simultaneous rotor failure detection and identification. The time-series assisted neural network is capable of making decisions throughout the entire flight with an accuracy of 98.8%, with minimum computation time (less than 0.03 s) making it the best alternative for real-time monitoring.

Reference

Dutta A., McKay ME., Kopsaftopoulos F.P., Gandhi F., " Multicopter Fault Detection and Identification via Data-Driven Statistical Learning Methods ,"

AIAA Journal, Vol. 60 (1), pp. 160-175, 2022.

Bibtex

@article{dutta2022multicopter,
  title={Multicopter Fault Detection and Identification via Data-Driven Statistical Learning Methods},
  author={Dutta, Airin and McKay, Michael E and Kopsaftopoulos, Fotis and Gandhi, Farhan},
  journal={AIAA Journal},
  volume={60},
  number={1},
  pages={160--175},
  year={2022},
  publisher={American Institute of Aeronautics and Astronautics}
}