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Modelling and Control of Mini-Flying Machines

Advances in Industrial Control

Erschienen am 21.10.2010, 1. Auflage 2005
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Bibliografische Daten
ISBN/EAN: 9781849969772
Sprache: Englisch
Umfang: xvi, 252 S., 126 s/w Illustr., 252 p. 126 illus.
Einband: kartoniertes Buch

Beschreibung

InhaltsangabeIntroduction and Historical Background The PVTOL Aircraft The Quad-rotor Rotorcraft Robust Prediction-based Control for Unstable Delay Systems Modelling and Control of mini-Helicopters Helicopter in a Vertical Flying Stand Modelling and Control of a Tandem-Wing Tail-Sitter UAV Modelling and Control of Small Autonomous Airships Sensors, Modems and Microcontrollers for UAVs Appendix A: Model Coefficients

Produktsicherheitsverordnung

Hersteller:
Springer Verlag GmbH
[email protected]
Tiergartenstr. 17
DE 69121 Heidelberg

Autorenportrait

Rogelio Lozano has worked in worked at a number of institutions with a high reputation for control engineering - the University of Newcastle in Australia, Nasa's Langley Research Center and now as CNRS Research Director at the University of Compiègne. He is a very experienced author in the control field being an associate editor of both Automatica and International Journal of Adaptive Control and Signal Processing. He is the co-author of 3 previous titles for Springer all of them in the Communications and Control Engineering series: Landau, I.D., Lozano, R. and M'Saad, M. Adaptive Control (1997) 3-540-76187-X Lozano, R., Brogliato, B., Egeland, O. and Maschke, B. Dissipative Systems Analysis and Control (1999) 1-85233-285-9 Fantoni, I. and Lozano, R. Non-linear Control for Underactuated Mechanical Systems (2001) 1-85233-423-1

Inhalt

Introduction and Historical Background The PVTOL Aircraft The Quad-rotor Rotorcraft Robust Prediction-based Control for Unstable Delay Systems Modelling and Control of mini-Helicopters Helicopter in a Vertical Flying Stand Modelling and Control of a Tandem-Wing Tail-Sitter UAV Modelling and Control of Small Autonomous Airships Sensors, Modems and Microcontrollers for UAVs Appendix A: Model Coefficients

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