An adaptive integral sliding mode FTC scheme for dissimilar redundant actuation system of civil aircraft

Keyphrases

• Control Allocation Scheme 100%
• Adaptive Integral Sliding Mode 100%
• Dissimilar Redundant Actuation System 100%
• Actuator Failure 100%
• Civil Aircraft 100%
• Law 50%
• Actuator Faults 50%
• Redundant Actuator 50%
• Actuator Effectiveness 50%
• Hydraulics 50%
• Adaptation Strategies 50%
• Actuator 50%
• Total Failure 50%
• Integral Sliding Mode Control 50%
• Unknown Actuator Faults 50%
• Modulation Gain 50%
• Dynamic Mismatch 50%
• Proposed Strategy 50%
• Control Control 50%
• Fault Condition 50%
• Electro-hydraulic Actuator 50%
• Fractional Order Controller 50%
• Reconstruction Scheme 50%
• Fault Reconstruction 50%
• Control Signal 50%
• Control Surface Deflection 50%
• Failure Control 50%
• Adaptive Modulation 50%
• Observer-based 50%
• Adaptive Sliding Mode Observer 50%
• Baseline Controller 50%

Engineering

• Actuation System 100%
• Sliding Mode 100%
• Civil Aircraft 100%
• Hydraulics 66%
• Fits and Tolerances 33%
• Sliding Mode Control 33%
• Actuator Failure 33%
• Control Surfaces 33%
• Adaptive Strategy 33%
• Control Signal 33%
• Fractional-Order Controller 33%