Zum Hauptinhalt springen
Nicht aus der Schweiz? Besuchen Sie lehmanns.de
Adverse Aeroelastic Rotorcraft-Pilot Couplings - Pierangelo Masarati, Giuseppe Quaranta

Adverse Aeroelastic Rotorcraft-Pilot Couplings

From Analysis to Prevention
Online Resource
125 Seiten
2024 | 1st ed. 2024
Springer International Publishing (Hersteller)
978-3-319-24451-8 (ISBN)
CHF 76,95 inkl. MwSt
  • Versand in 10-14 Tagen
  • Versandkostenfrei
  • Auch auf Rechnung
  • Artikel merken
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
Themenwelt Technik Luft- / Raumfahrttechnik
Schlagworte Biodynamic Feedthrough • multibody dynamics • Pilot-Augmented Oscillations • Pilot Biomechanics • Pilot-Induced Oscillations • Pilot-Vehicle Interaction • Robust Stability • Rotorcraft Aeromechanics • Rotorcraft-Pilot Couplings
ISBN-10 3-319-24451-5 / 3319244515
ISBN-13 978-3-319-24451-8 / 9783319244518
Zustand Neuware
Informationen gemäß Produktsicherheitsverordnung (GPSR)
Haben Sie eine Frage zum Produkt?