Event-triggered fixed-time fault-tolerant attitude control for the flying-wing UAV using a Nussbaum-type function

Computer Science

• actuator fault 33%
• Control Approach 33%
• Control Framework 33%
• Fault Tolerant 100%
• Numerical Simulation 33%
• radial base function neural network 33%
• Sampling Error 33%
• Triggered Event 100%
• Unmanned Aerial Vehicle 100%

Engineering

• Actuator Failure 33%
• Attitude Control 100%
• Computer Simulation 33%
• Control System 33%
• External Disturbance 33%
• Feedback Control System 33%
• Frame Time 33%
• Radial Basis Function 33%
• Sampling Error 33%
• Singularities 33%
• Unmanned Aerial Vehicle 100%