Anbieter: Majestic Books, Hounslow, Vereinigtes Königreich
EUR 15,32
Anzahl: 4 verfügbar
In den WarenkorbZustand: New.
Verlag: The Institution of Engineering and Technology, 2000
ISBN 10: 0852967667 ISBN 13: 9780852967669
Sprache: Englisch
Anbieter: Phatpocket Limited, Waltham Abbey, HERTS, Vereinigtes Königreich
EUR 104,89
Anzahl: 1 verfügbar
In den WarenkorbZustand: Good. Your purchase helps support Sri Lankan Children's Charity 'The Rainbow Centre'. Ex-library, so some stamps and wear, but in good overall condition. Our donations to The Rainbow Centre have helped provide an education and a safe haven to hundreds of children who live in appalling conditions.
Taschenbuch. Zustand: Neu. Flight Systems and Control | A Practical Approach | Tian Seng Ng | Taschenbuch | xxiii | Englisch | 2018 | Springer Singapore | EAN 9789811342233 | Verantwortliche Person für die EU: Springer Verlag GmbH, Tiergartenstr. 17, 69121 Heidelberg, juergen[dot]hartmann[at]springer[dot]com | Anbieter: preigu.
Verlag: Springer Nature Singapore, Springer Nature Singapore, 2018
ISBN 10: 9811342237 ISBN 13: 9789811342233
Sprache: Englisch
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Taschenbuch. 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: Revaluation Books, Exeter, Vereinigtes Königreich
EUR 218,49
Anzahl: 1 verfügbar
In den WarenkorbPaperback. Zustand: Brand New. reprint edition. 272 pages. 9.25x6.10x0.67 inches. In Stock.
Verlag: Springer London, Springer London, 2010
ISBN 10: 1849968500 ISBN 13: 9781849968508
Sprache: Englisch
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Taschenbuch. 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.
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Buch. 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.
Verlag: Springer Nature Singapore, Springer Nature Singapore, 2018
ISBN 10: 9811087202 ISBN 13: 9789811087202
Sprache: Englisch
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Buch. 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: Institution Of Engineering & Technology Jun 2000, 2000
ISBN 10: 0852967667 ISBN 13: 9780852967669
Sprache: Englisch
Anbieter: AHA-BUCH GmbH, Einbeck, Deutschland
Buch. 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.
Anbieter: Revaluation Books, Exeter, Vereinigtes Königreich
EUR 274,32
Anzahl: 2 verfügbar
In den WarenkorbHardcover. Zustand: Brand New. 268 pages. 9.50x6.50x0.75 inches. In Stock.