Integrated flight control design for a large flexible aircraft

Keyphrases

• Flexible Aircraft 100%
• Flight Control Design 100%
• Rigid Body 50%
• Controller 50%
• Linear Parameter Varying 50%
• Flight Control System 50%
• Mode Control 50%
• Design Procedure 50%
• Handling Qualities 50%
• Nonlinear Model 50%
• Systematic Design 50%
• Structural Vibration 50%
• Body Control 50%
• Control Configuration 50%
• Robustness Margin 50%
• Structural Mode 50%
• Control Objectives 50%
• Conventional Controller 50%
• Mixed Sensitivity 50%
• Aeroelastic Control 50%
• Stability Augmentation 50%
• Integrated Controller 50%
• Two-degree-of-freedom Control 50%
• Modal Representation 50%

Engineering

• Flight Control 100%
• Control Design 100%
• Aeroelastic Control 50%
• Rigid Structure 50%
• Design Procedure 50%
• Applicability 50%
• Structural Vibration 50%
• Two Degree of Freedom 50%
• Mode Control 50%
• Nonlinear Model 50%
• Control Objective 50%
• Configuration Control 50%
• Stability Augmentation 50%
• Controllability 50%