Robust aeroelastic control of flapped wing systems using a sliding mode observer

Keyphrases

• Sliding Mode Observer 100%
• Aeroelastic Control 100%
• Flight Speed 100%
• Flutter Instability 50%
• Vibrational Levels 50%
• Control Method 50%
• Flap 50%
• Linear Quadratic Gaussian Control 50%
• Aeroelastic System 50%
• Robust Control Strategy 50%
• Pressure Pulse 50%
• Three Degrees of Freedom 50%
• Speed Range 50%
• Linear Quadratic Gaussian Controller 50%
• Standard Kalman Filter 50%

Engineering

• Sliding Mode 100%
• Linear Quadratic Gaussian 100%
• Aeroelastic Control 100%
• Kalman Filter 50%
• Degree of Freedom 50%
• Control Strategy 50%
• Flaps 50%