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This book offers a complete overview of fault-tolerant flight control techniques. Discussion covers the necessary equations for the modeling of small UAVs, a complete system based on extended Kalman filters, and a nonlinear flight control and guidance system.
Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.
EUR 23 expédition depuis Allemagne vers Etats-Unis
Destinations, frais et délaisVendeur : BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Allemagne
Buch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Unmanned aerial vehicles (UAVs) offer an incomparable means of gathering intelligence and carrying out missions without needing an onboard human pilot. The benefits are considerable in terms of cost, efficiency, and reduced pilot risk.In order to complete a mission efficiently and with a high level of safety and security, the following key design points must be met:- the flight control system must be robust against the aircraft's model uncertainties and external disturbances;- an efficient fault detection and isolation (FDI) system should be capable of monitoring the health of the aircraft; and- the flight control and guidance system should be reconfigurable depending on actuator fault occurrence or aircraft damage, and should be able to avoid obstacles.Fault-tolerant Flight Control and Guidance Systems addresses all of these aspects with a practical approach following three main requirements: being applicable in real-time; highly computationally efficient; and modular. The text provides:- an overview of fault-tolerant flight control techniques;- the necessary equations for the modeling of small UAVs;- a complete nonlinear FDI system based on extended Kalman filters; and- a nonlinear flight control and guidance system.The book is written in a didactic style with many figures and diagrams making it suitable not only for academic researchers and practicing engineers but also graduate students working in the fields of fault detection techniques and the automatic control of UAVs. 268 pp. Englisch. N° de réf. du vendeur 9781848825604
Quantité disponible : 2 disponible(s)
Vendeur : Ria Christie Collections, Uxbridge, Royaume-Uni
Etat : New. In. N° de réf. du vendeur ria9781848825604_new
Quantité disponible : Plus de 20 disponibles
Vendeur : moluna, Greven, Allemagne
Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Gives the reader a complete overview of fault-tolerant flight control techniques including modeling equations and extended Kalman filter implementationPresents a complete nonlinear flight control system with many figures and finite-state diagrams . N° de réf. du vendeur 4287059
Quantité disponible : Plus de 20 disponibles
Vendeur : AHA-BUCH GmbH, Einbeck, Allemagne
Buch. Etat : Neu. Druck auf Anfrage Neuware - Printed after ordering - Unmanned aerial vehicles (UAVs) offer an incomparable means of gathering intelligence and carrying out missions without needing an onboard human pilot. The benefits are considerable in terms of cost, efficiency, and reduced pilot risk.In order to complete a mission efficiently and with a high level of safety and security, the following key design points must be met:- the flight control system must be robust against the aircraft's model uncertainties and external disturbances;- an efficient fault detection and isolation (FDI) system should be capable of monitoring the health of the aircraft; and- the flight control and guidance system should be reconfigurable depending on actuator fault occurrence or aircraft damage, and should be able to avoid obstacles.Fault-tolerant Flight Control and Guidance Systems addresses all of these aspects with a practical approach following three main requirements: being applicable in real-time; highly computationally efficient; and modular. The text provides:- an overview of fault-tolerant flight control techniques;- the necessary equations for the modeling of small UAVs;- a complete nonlinear FDI system based on extended Kalman filters; and- a nonlinear flight control and guidance system.The book is written in a didactic style with many figures and diagrams making it suitable not only for academic researchers and practicing engineers but also graduate students working in the fields of fault detection techniques and the automatic control of UAVs. N° de réf. du vendeur 9781848825604
Quantité disponible : 2 disponible(s)