Adverse Aeroelastic Rotorcraft-Pilot Couplings
From Analysis to Prevention
Seiten
2024
|
1st ed. 2024
Springer International Publishing (Verlag)
978-3-319-24449-5 (ISBN)
Springer International Publishing (Verlag)
978-3-319-24449-5 (ISBN)
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This book presents methods for the analysis of rotorcraft-pilot couplings, discusses typical phenomena, and suggests ways to predict and reduce adverse coupling events at the design stage. The book is divided into three parts; the first offers an introduction to a "modern" approach to the modeling of complex systems applied to rotorcraft aeromechanics, pilot biomechanics, and their interaction, namely biodynamic feedthrough. The second part presents a general approach for simulation of the coupled pilot-vehicle system and analyzes specific stability problems in detail. The final part focuses specifically on alleviation and prevention of adverse rotorcraft-pilot couplings with the aim of designing a cockpit with reduced sensitivity to biodynamic feedthrough. It explains how robust stability analysis can improve the design of the pilot-vehicle interface and how simple parametric models can assist in designing tuned impedance control devices that will increase the robustness of the coupled pilot-vehicle system.
Introduction.- Multibody System Dynamics.- A Modern Approach to Rotorcraft Modeling.- Cognitive and Biomechanical Pilot Modeling.- Coupled Pilot-Vehicle Analysis.- Collective Bounce.- Roll Instability.- Robust Stability Analysis.- Tuned Control Devices.- Towards Future Cockpit Design.
Erscheint lt. Verlag | 14.2.2024 |
---|---|
Zusatzinfo | 125 p. 50 illus. |
Verlagsort | Cham |
Sprache | englisch |
Maße | 155 x 235 mm |
Themenwelt | Technik ► Luft- / Raumfahrttechnik |
Schlagworte | Aerospace Technology and Astronautics • Biodynamic Feedthrough • biomedical engineering • Engineering • fluid- and aerodynamics • multibody dynamics • Pilot-Augmented Oscillations • Pilot Biomechanics • Pilot-Induced Oscillations • Pilot-Vehicle Interaction • Robust Stability • Rotorcraft Aeromechanics • Rotorcraft-Pilot Couplings • Vibration, Dynamical Systems, Control |
ISBN-10 | 3-319-24449-3 / 3319244493 |
ISBN-13 | 978-3-319-24449-5 / 9783319244495 |
Zustand | Neuware |
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