Adaptive control laws for flexible semi-span wind tunnel model of high-aspect ratio flying wing

Keyphrases

• High Aspect Ratio 100%
• Controller 100%
• L1 Adaptive Controller 100%
• Adaptive Control Law 100%
• Altitude Hold 100%
• Gust Load Alleviation 100%
• Wind Tunnel Model 100%
• Flying Wing 100%
• Rigid Body Motion 50%
• Mode Coupling 50%
• Wind Tunnel 50%
• Control Architecture 50%
• Rigid Body 50%
• Response Performance 50%
• Extra Degree of Freedom 50%
• Output Feedback 50%
• Control Objectives 50%
• Swept Wing 50%
• Nominal Controller 50%
• Flutter Suppression 50%
• Pitch Control 50%
• Controller Development 50%
• Span-based Model 50%
• Flexible Modes 50%
• Stability Augmentation System 50%
• Adaptive Loop 50%
• Aircraft Configuration 50%
• Body Freedom Flutter 50%

Engineering

• Adaptive Control 100%
• High Aspect Ratio 100%
• Control Law 100%
• Gust Loads 100%
• Altitude Hold 100%
• Rigid Body Motion 50%
• Degree of Freedom 50%
• Rigid Structure 50%
• Control Architecture 50%
• Additional Degree 50%
• Adaptive Controller 50%
• Output Feedback 50%
• Control Objective 50%
• Swept Wings 50%
• Pitch Control 50%
• Augmentation System 50%
• Stability Augmentation 50%
• Model Position 50%