Active fault-tolerant control for vertical tail damaged aircraft with dissimilar redundant actuation system using integral sliding mode control

Keyphrases

• Dissimilar Redundant Actuation System 100%
• Actuator 100%
• Integral Sliding Mode Control 100%
• Active Fault-tolerant Control 100%
• Vertical Tail 100%
• Damaged Aircraft 100%
• Electro-hydraulic Actuator 75%
• Control Strategy 50%
• Hydraulic Actuator 50%
• Severe Damage 50%
• Severe Disease 25%
• Controller 25%
• Design Methodology 25%
• Performance Degradation 25%
• Fault-tolerant Control 25%
• Actuator Faults 25%
• Fault Estimation 25%
• Actuator Effectiveness 25%
• Closed-loop Stability 25%
• Integral Sliding Mode Controller 25%
• Fault-tolerant 25%
• Proposed Design 25%
• Actuator Failure 25%
• Modern Aircraft 25%
• Slow Dynamics 25%
• Proposed Strategy 25%
• Online Control Allocation 25%
• Control Signal 25%
• Active Switching 25%
• Fractional Order Control 25%
• Switching Mechanism 25%
• Actuator Saturation 25%
• Damage Condition 25%
• Vertical Tail Damage 25%
• Component Faults 25%
• Potential Faults 25%
• Feedforward Compensator 25%

Engineering

• Actuation System 100%
• Fault Tolerant Control 100%
• Sliding Mode Control 100%
• Control Strategy 100%
• Hydraulics 100%
• Severe Damage 100%
• Simulation Result 50%
• Closed Loop 50%
• Performance Degradation 50%
• Loop Stability 50%
• Sliding Mode Controller 50%
• Actuator Failure 50%
• Fractional-Order 50%
• Feedforward 50%
• Control Signal 50%
• Damage Condition 50%