Könyv Flight Dynamics and System Identification for Modern Feedback Control James E. Hubbard

Flight Dynamics and System Identification for Modern Feedback Control

Avian-Inspired Robots

Nyelv: Angol
Kötés: Kemény kötésű
Elérhetőség: Kiadói készleten rendelésre
Küldés 28-34 napon belül
55 300 Ft
Unmanned air vehicles are becoming increasingly popular alternatives for private applications which...

Információk a könyvről

Nyelv
Angol
Kötés
Könyv - Kemény kötésű
Kiadva
2013
oldal
160
EAN
9780857094667
ISBN
0857094661
Enbook ID
04741990
Súly
386
Méretek
157 x 240 x 15

Teljes leírás

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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