Adaptive integral-sliding-mode control strategy for maneuvering control of F16 aircraft subject to aerodynamic uncertainty

Keyphrases

• Sliding Mode Control Method 100%
• Maneuver Control 100%
• Nonlinear Dynamic Inversion 100%
• Aerodynamic Uncertainty 100%
• Dynamic Inversion Control 100%
• Adaptive Integral Sliding Mode Control 100%
• System Stability 33%
• Unknown Disturbances 33%
• Adaptive Integral Sliding Mode 33%
• Adaptation Strategies 33%
• Flight Data 33%
• Design Objectives 33%
• Control Approach 33%
• Nonlinear Dynamics 33%
• Wind Tunnel 33%
• Time-scale Separation 33%
• High Angle of Attack 33%
• Fighter Aircraft 33%
• Least Square Algorithm 33%
• Aerodynamic Coefficients 33%
• Nonlinear Control 33%
• Aircraft Dynamics 33%
• Separation Principle 33%
• Flight Quality 33%
• Highly Nonlinear 33%
• Nonlinear Dynamic Inversion Control 33%
• Disturbance Uncertainties 33%
• Dynamic Stability 33%
• Real-time Performance 33%
• Integral Sliding Mode 33%
• Internal Dynamics 33%
• Iteratively Reweighted Least Squares (IRWLS) 33%
• Two-loop 33%
• Robust Adaptive 33%
• Performance Ability 33%
• Flight Controller 33%
• Complete System 33%

Engineering

• Sliding Mode Control 100%
• Control Strategy 100%
• Non-Linear Dynamic 100%
• Sliding Mode 40%
• Systems Stability 20%
• Least Square 20%
• Flight Data 20%
• Design Objective 20%
• NASA 20%
• Fighter Aircraft 20%
• Dynamic Stability 20%
• Complete System 20%
• Internal Dynamic 20%
• Aerodynamic Coefficient 20%
• Angle-of-Attack 20%
• Adaptive Strategy 20%