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Adaptive Fault-Tolerant Control of a Hybrid Canard Rotor/Wing UAV Under Transition Flight Subject to Actuator Faults and Model Uncertainties.

Ban WangDehai ZhuLinying HanHonggang GaoZhenghong GaoYoumin Zhang
Published in: IEEE Trans. Aerosp. Electron. Syst. (2023)
Keyphrases
  • mathematical model
  • experimental data
  • neural network
  • mobile robot
  • reliability analysis
  • pattern recognition
  • expert systems
  • state space
  • fuzzy logic
  • fault diagnosis
  • linear model
  • flight data