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Flight dynamics and system identification for modern feedback control: Avian-inspired Robots - Rilegato

 
9780857094667: Flight dynamics and system identification for modern feedback control: Avian-inspired Robots

Sinossi

Unmanned air vehicles are becoming increasingly popular alternatives for private applications which include, but are not limited to, fire fighting, search and rescue, atmospheric data collection, and crop surveys, to name a few. Among these vehicles are avian-inspired, flapping-wing designs, which are safe to operate near humans and are required to carry payloads while achieving manoeuverability and agility in low speed flight. Conventional methods and tools fall short of achieving the desired performance metrics and requirements of such craft. Flight dynamics and system identification for modern feedback control provides an in-depth study of the difficulties associated with achieving controlled performance in flapping-wing, avian-inspired flight, and a new model paradigm is derived using analytical and experimental methods, with which a controls designer may then apply familiar tools. This title consists of eight chapters and covers flapping-wing aircraft and flight dynamics, before looking at nonlinear, multibody modelling as well as flight testing and instrumentation. Later chapters examine system identification from flight test data, feedback control and linearization.

  • Presents experimental flight data for validation and verification of modelled dynamics, thus illustrating the deficiencies and difficulties associated with modelling flapping-wing flight
  • Derives a new flight dynamics model needed to model avian-inspired vehicles, based on nonlinear multibody dynamics
  • Extracts aerodynamic models of flapping flight from experimental flight data and system identification techniques

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Recensione

"...very clearly written and is quite readable. The authors are clearly leading experts in the field...strongly recommended to readers interested in the subject."--The Aeronautical Journal, February 2015

"Aerospace engineers Grauer...and Hubbard...describe an ornithopter they designed, built, and tested. An ornithopter flies by flapping wings like a bird. They cover ornithopter test platform characterizations, rigid multi-body vehicle dynamics, system identification of aerodynamic models, and simulation results."--ProtoView.com, February 2014

L'autore

Jared A. Grauer is a research aerospace engineer with the National Aeronautics and Space Administration at Langley Research Center. Prior to this he earned a PhD from the University of Maryland in Aerospace Engineering. His research is in system identification, feedback control, and unmanned air vehicle systems.

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  • EditoreWoodhead Pub Ltd
  • Data di pubblicazione2013
  • ISBN 10 0857094661
  • ISBN 13 9780857094667
  • RilegaturaCopertina rigida
  • LinguaInglese
  • Numero edizione1
  • Numero di pagine138

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Jared A. Grauer,James E. Hubbard Jr.
ISBN 10: 0857094661 ISBN 13: 9780857094667
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Hardcover. Condizione: New. Codice articolo 6666-ELS-9780857094667

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Hubbard Jr. J E Grauer J A Hubbard J. E. Grauer J. A.
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J E Hubbard Jr. J A Grauer J. E. Hubbard J. A. Grauer
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Grauer, Jared/ Hubbard, James
Editore: Woodhead Pub Ltd, 2013
ISBN 10: 0857094661 ISBN 13: 9780857094667
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Hubbard Jr. J E Grauer J A Hubbard J. E. Grauer J. A.
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Jared A Grauer
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Buch. Condizione: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Unmanned air vehicles are becoming increasingly popular alternatives for private applications which include, but are not limited to, fire fighting, search and rescue, atmospheric data collection, and crop surveys, to name a few. Among these vehicles are avian-inspired, flapping-wing designs, which are safe to operate near humans and are required to carry payloads while achieving manoeuverability and agility in low speed flight. Conventional methods and tools fall short of achieving the desired performance metrics and requirements of such craft. Flight dynamics and system identification for modern feedback control provides an in-depth study of the difficulties associated with achieving controlled performance in flapping-wing, avian-inspired flight, and a new model paradigm is derived using analytical and experimental methods, with which a controls designer may then apply familiar tools. This title consists of eight chapters and covers flapping-wing aircraft and flight dynamics, before looking at nonlinear, multibody modelling as well as flight testing and instrumentation. Later chapters examine system identification from flight test data, feedback control and linearization. Englisch. Codice articolo 9780857094667

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Buch. Condizione: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Unmanned air vehicles are becoming increasingly popular alternatives for private applications which include, but are not limited to, fire fighting, search and rescue, atmospheric data collection, and crop surveys, to name a few. Among these vehicles are avian-inspired, flapping-wing designs, which are safe to operate near humans and are required to carry payloads while achieving manoeuverability and agility in low speed flight. Conventional methods and tools fall short of achieving the desired performance metrics and requirements of such craft. Flight dynamics and system identification for modern feedback control provides an in-depth study of the difficulties associated with achieving controlled performance in flapping-wing, avian-inspired flight, and a new model paradigm is derived using analytical and experimental methods, with which a controls designer may then apply familiar tools. This title consists of eight chapters and covers flapping-wing aircraft and flight dynamics, before looking at nonlinear, multibody modelling as well as flight testing and instrumentation. Later chapters examine system identification from flight test data, feedback control and linearization. Codice articolo 9780857094667

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