Dynamics and active feedback control of wing-type structures modeled as thin-walled beams: implications of beam cross-section nonuniformity

Keyphrases

• Thin-walled Beam 100%
• Non-uniformity 100%
• Aircraft Wing 100%
• Dynamic Feedback Control 100%
• Active Feedback Control 100%
• Beam Cross Section 100%
• Wing Shape 100%
• Numerical Results 50%
• Transverse Shear 50%
• External Excitation 50%
• Cantilever 50%
• Boundary Moment 50%
• Dynamic Response 50%
• Moment Control 50%
• Feedback Control 50%
• Robotic Manipulator 50%
• Tapered Thin-walled Beam 50%
• Dynamical Behavior 50%
• Open-closed-loop 50%
• Free Vibration Response 50%
• Taper Ratio 50%
• Loop-free 50%
• Transverse Shear Effects 50%
• Vibration Feedback 50%
• Chimney 50%
• Helicopter Blade 50%
• Large Category 50%

Engineering

• Wings 100%
• Structure Type 100%
• Beam Cross Section 100%
• Feedback Control 100%
• Illustrates 50%
• Dynamic Response 50%
• Closed Loop 50%
• Robotic Manipulator 50%
• Helicopter Blade 50%
• Dynamical Behavior 50%
• Free Vibration 50%