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Verlag: Allied Publishers Pvt. Ltd. Allied
ISBN 10: 9387997812 ISBN 13: 9789387997813
Sprache: Englisch
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In den WarenkorbZustand: New.
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In den WarenkorbZustand: As New. Unread book in perfect condition.
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In den WarenkorbZustand: As New. Unread book in perfect condition.
Verlag: Iet, 2012
Sprache: Englisch
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In den WarenkorbN.A. Zustand: New. ISBN:9780852967669,Territorial restriction maybe printed on the book. This is an Int'l edition, ISBN and cover may differ from US edition, Contents same as US edition.
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In den WarenkorbHardcover. Zustand: New. New. book.
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In den WarenkorbZustand: New. In.
Verlag: Springer Nature Singapore, Springer Nature Singapore, 2018
ISBN 10: 9811342237 ISBN 13: 9789811342233
Sprache: Englisch
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In den WarenkorbTaschenbuch. Zustand: Neu. Druck auf Anfrage Neuware - Printed after ordering - This book focuses on flight vehicles and their navigational systems, discussing different forms of flight structures and their control systems, from fixed wings to rotary crafts. Software simulation enables testing of the hardware without actual implementation, and the flight simulators, mechanics, glider development and navigation systems presented here are suitable for lab-based experimentation studies. It explores laboratory testing of flight navigational sensors, such as the magnetic, acceleration and Global Positioning System (GPS) units, and illustrates the six-axis inertial measurement unit (IMU) instrumentation as well as its data acquisition methodology. The book offers an introduction to the various unmanned aerial vehicle (UAV) systems and their accessories, including the linear quadratic regulator (LQR) method for controlling the rotorcraft. It also describes a Matrix Laboratory (MATLAB) control algorithm that simulates and runs the lab-based 3 degrees of freedom (DOF) helicopter, as well as LabVIEW software used to validate controller design and data acquisition. Lastly, the book explores future developments in aviation techniques.
Verlag: Springer London, Springer London, 2010
ISBN 10: 1849968500 ISBN 13: 9781849968508
Sprache: Englisch
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In den WarenkorbTaschenbuch. Zustand: 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.
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In den WarenkorbBuch. Zustand: 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.
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In den WarenkorbZustand: New. In.
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In den WarenkorbZustand: New.
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In den WarenkorbZustand: New.
Verlag: Springer Nature Singapore, Springer Nature Singapore, 2018
ISBN 10: 9811087202 ISBN 13: 9789811087202
Sprache: Englisch
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In den WarenkorbBuch. Zustand: Neu. Druck auf Anfrage Neuware - Printed after ordering - This book focuses on flight vehicles and their navigational systems, discussing different forms of flight structures and their control systems, from fixed wings to rotary crafts. Software simulation enables testing of the hardware without actual implementation, and the flight simulators, mechanics, glider development and navigation systems presented here are suitable for lab-based experimentation studies. It explores laboratory testing of flight navigational sensors, such as the magnetic, acceleration and Global Positioning System (GPS) units, and illustrates the six-axis inertial measurement unit (IMU) instrumentation as well as its data acquisition methodology. The book offers an introduction to the various unmanned aerial vehicle (UAV) systems and their accessories, including the linear quadratic regulator (LQR) method for controlling the rotorcraft. It also describes a Matrix Laboratory (MATLAB) control algorithm that simulates and runs the lab-based 3 degrees of freedom (DOF) helicopter, as well as LabVIEW software used to validate controller design and data acquisition. Lastly, the book explores future developments in aviation techniques.
Anbieter: dsmbooks, Liverpool, Vereinigtes Königreich
EUR 180,72
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In den WarenkorbPaperback. Zustand: New. New. book.
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In den WarenkorbPaperback. Zustand: Brand New. reprint edition. 272 pages. 9.25x6.10x0.67 inches. In Stock.
Verlag: Institution Of Engineering & Technology Jun 2000, 2000
ISBN 10: 0852967667 ISBN 13: 9780852967669
Sprache: Englisch
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In den WarenkorbBuch. Zustand: Neu. Neuware - A complete reference on modern flight control methods for fixed-wing aircraft, this authoritative book includes contributions from an international group of experts in their respective specialised fields, largely from industry.
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In den WarenkorbZustand: New.
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In den WarenkorbPaperback. Zustand: Like New. Like New. book.
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In den WarenkorbHardcover. Zustand: New. New. book.
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In den WarenkorbHardcover. Zustand: Brand New. 268 pages. 9.50x6.50x0.75 inches. In Stock.
Verlag: National Defense Industry Press, 2012
ISBN 10: 7118077232 ISBN 13: 9787118077230
Sprache: Chinesisch
Anbieter: liu xing, Nanjing, JS, China
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In den WarenkorbHardcover. Zustand: New. Ship out in 2 business day, And Fast shipping, Free Tracking number will be provided after the shipment.HardCover. Pub Date :2012-05-01 Publisher: National Defense Industry Press circulation department only genuine brand new book No pictures. Baidu check title ISBN Pricing Press; only puerile - not counteroffer not free open textbook amount of the invoice is not taxed. books dedicated machine-printed invoices.Four Satisfaction guaranteed,or money back.
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In den WarenkorbPaperback / softback. Zustand: New. This item is printed on demand. New copy - Usually dispatched within 5-9 working days 466.
Anbieter: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, Deutschland
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In den WarenkorbBuch. Zustand: 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.
Anbieter: Majestic Books, Hounslow, Vereinigtes Königreich
EUR 183,31
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In den WarenkorbZustand: New. Print on Demand.
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In den WarenkorbZustand: New. PRINT ON DEMAND.