"...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
"Sobre este título" puede pertenecer a otra edición de este libro.
Gastos de envío:
EUR 11,66
De Reino Unido a Estados Unidos de America
Descripción Hardcover. Condición: Brand New. 138 pages. 9.25x6.25x0.75 inches. In Stock. Nº de ref. del artículo: __0857094661
Descripción Condición: new. Questo è un articolo print on demand. Nº de ref. del artículo: 5820a3548bedf73136756539e6df63b4
Descripción Hardback. Condición: New. New copy - Usually dispatched within 4 working days. Nº de ref. del artículo: B9780857094667
Descripción Buch. Condición: 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. Nº de ref. del artículo: 9780857094667
Descripción Condición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. 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 analytic. Nº de ref. del artículo: 595101472
Descripción Buch. Condición: 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. Nº de ref. del artículo: 9780857094667
Descripción Hardcover. Condición: New. Nº de ref. del artículo: 6666-ELS-9780857094667