Review of algorithms and comparative study of controllers for damping the aircraft aeroelastic vibrations

Key Points

• The review aims to evaluate existing algorithms and controllers used for damping aeroelastic vibrations in aircraft.
• Conducted comparative analysis of various control algorithms for aircraft
• Evaluated performance metrics of different controllers in minimizing vibrations
• Assessed the effectiveness of damping techniques on aircraft dynamics.
• Identified key algorithms that significantly reduce aeroelastic vibrations
• Demonstrated the superiority of adaptive controllers over traditional methods
• Highlighted the need for continued research to optimize vibration control solutions.