Finite Time Convergence Incremental Nonlinear Dynamic Inversion Based Attitude Control for Flying - Wing Aircraft with Actuator Faults.
Wuhan HanShaojie ZhangPublished in: CAA SAFEPROCESS (2019)
Keyphrases
- nonlinear dynamics
- control system
- neural network
- control method
- air fuel ratio
- fault diagnosis
- vision system
- dynamical systems
- convergence rate
- reinforcement learning
- image reconstruction
- attitudes toward
- test cases
- fault detection
- fuzzy logic
- nasa langley research center
- dc motor
- iterative learning control
- guaranteed cost