Design of a tolerant flight control system in response to multiple actuator control signal faults induced by cosmic rays

Keyphrases

• Actuator 40%
• Actuator Control 100%
• Aircraft Performance 20%
• Avionics System 20%
• Closed-loop System Stability 20%
• Control Signal 100%
• Cosmic Ray Particles 20%
• Cosmic Rays 100%
• Detection Method 20%
• Diagnostic Methods 20%
• Double Fault 20%
• Fault Detection 20%
• Fault Diagnosis 20%
• Fault-tolerant Flight Control 20%
• Faulty Actuator 20%
• Flight Control System 100%
• Flyby 40%
• Geometric Approach 20%
• Healthy Controls 20%
• High Performance 20%
• High-altitude Flight 20%
• Lyapunov Theory 20%
• MATLAB Simulink 20%
• Microelectronics 20%
• Miniaturization 20%
• Multiple Actuators 100%
• Multiple Bit Upsets 20%
• Multiple Model Adaptive Estimation 20%
• Novel Architecture 20%
• Reconfigurable 20%
• Semiconductors 20%
• Sensor Noise 20%
• Sliding Mode Control 20%
• Solar Particle Events 20%
• Systems-based 20%

Engineering

• Actuator 100%
• Aircraft Performance 16%
• Avionics 16%
• Closed-Loop System Stability 16%
• Control Signal 100%
• Fault Detection and Diagnosis 16%
• Flight Control 100%
• Healthy Control 16%
• High-Altitude Flight 16%
• Lyapunov Stability Theory 16%
• Matlab-Simulink 16%
• Microelectronics 16%
• Sensor Noise 16%
• Simulation Result 16%
• Sliding Mode Control 16%