Aeromechanical Stability Augmentation Through Semi-Active Control | Semi-Active Friction based Damping for Rotorcraft Ground Resonance Stability

Sandeep Agarwal

ISBN 10: 3639175328 / ISBN 13: 9783639175325

Published by VDM Verlag Dr. Müller, 2009

About this Item

Aeromechanical Stability Augmentation Through Semi-Active Control | Semi-Active Friction based Damping for Rotorcraft Ground Resonance Stability | Sandeep Agarwal | Taschenbuch | Englisch | VDM Verlag Dr. Müller | EAN 9783639175325 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu.

Seller Inventory # 101522117

Bibliographic Details

• Title: Aeromechanical Stability Augmentation Through Semi-Active Control | Semi-Active Friction based Damping for Rotorcraft Ground Resonance Stability
• Publisher: VDM Verlag Dr. Müller
• Publication Date: 2009
• Language: English
• ISBN 10: 3639175328
• ISBN 13: 9783639175325
• Binding: Taschenbuch
• Condition: Neu
• Seller catalogs:
  • Bücher

About this title

Synopsis

Helicopter rotors have traditionally been equipped with passive dampers for aeromechanical stability. These passive systems have fixed characteristics, and add to mechanical complexity and high maintenance cost. Furthermore, they are unable to change to compensate for an unexpected loading trends as typically encountered by a rotary wing vehicle. Semi-active control strategies are dissipative in nature, inherently stable, and require a little energy to operate. Hence, they appear to be particularly promising in addressing a number of the challenges facing active control strategies, in that the devices are low power, fail-safe, and reliable. In this study, author investigates friction based semi-active approach for ground resonance stability augmentation and proposes novel strategies for the adaptive, selective and individual damping control. The effectiveness of these control strategies is validated on a comprehensive multibody system model of an army helicopter. The analytical study is supplemented with a novel design of a semi-active lead lag damper and various aspects of its design in application to commercial rotors are discussed.

About the Author

Dr. Sandeep Agarwal is a Rotor Dynamics Engineer at the Boeing Company. Prior to that, he worked at the Center of Excellence in Rotorcraft Technology at Georgia Institute of Technology. His primary interests include Rotor dynamics, Aeroelasticity, Structural Morphing and Structural Optimization. He has authored several technical publications.