Linear, parameter varying model reduction for aeroservoelastic systems

Keyphrases

• Active Flutter Suppression 20%
• Aeroservoelastic 100%
• Balanced Realization 60%
• Bending Mode 40%
• Body Freedom Flutter 80%
• Consistent State 20%
• Controller 20%
• Controller Design 20%
• Flight Envelope 40%
• Flutter Model 20%
• High-lying States 20%
• Linear Parameter Varying 100%
• Model Order Reduction 20%
• Model Reduction 100%
• Model States 20%
• Operating Conditions 40%
• Order Reduction 20%
• Ordered Models 20%
• Parameter-varying 20%
• Residualisation 20%
• Rigid Body Dynamics 20%
• State Capture 20%
• State Model 20%
• State Order 20%
• State-space Model 20%
• Synthetic Control Method 20%
• Torsional Mode 20%
• Truncation 20%
• Vehicle Dynamics 20%

Engineering

• Balanced Realization 100%
• Control Synthesis 33%
• Controller Design 33%
• Design Result 33%
• Flight Envelope 66%
• Model Reduction 100%
• Rigid Structure 33%
• State Model 66%
• Truncation 33%
• Vehicle Dynamics 33%