Dynamic inversion fuzzy integration control in high angle-of-attack flight

Engineering

• Angle-of-Attack 100%
• Pitch Rate 100%
• Outer Loop 100%
• Fuzzy Controller 100%
• Design Method 50%
• Simulation Result 50%
• Control Surface 50%
• Control Design 50%
• Flight Condition 50%
• Controllability 50%
• Model Uncertainty 50%
• Loop Dynamic 50%
• Aerodynamic Control 50%