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000838618 019__ $$a1031916633$$a1031959380$$a1032024869$$a1032144740$$a1034546699$$a1038452076
000838618 020__ $$a9789811087219$$q(electronic book)
000838618 020__ $$a9811087210$$q(electronic book)
000838618 020__ $$z9789811087202
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000838618 0247_ $$a10.1007/978-981-10-8721-9$$2doi
000838618 035__ $$aSP(OCoLC)on1031377224
000838618 035__ $$aSP(OCoLC)1031377224$$z(OCoLC)1031916633$$z(OCoLC)1031959380$$z(OCoLC)1032024869$$z(OCoLC)1032144740$$z(OCoLC)1034546699$$z(OCoLC)1038452076
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000838618 049__ $$aISEA
000838618 050_4 $$aTL589.4
000838618 08204 $$a629.132/6$$223
000838618 1001_ $$aNg, Tian Seng,$$eauthor.
000838618 24510 $$aFlight systems and control :$$ba practical approach /$$cTian Seng Ng.
000838618 264_1 $$aSingapore :$$bSpringer,$$c2018.
000838618 300__ $$a1 online resource (xxiii, 241 pages) :$$billustrations.
000838618 336__ $$atext$$btxt$$2rdacontent
000838618 337__ $$acomputer$$bc$$2rdamedia
000838618 338__ $$aonline resource$$bcr$$2rdacarrier
000838618 347__ $$atext file$$bPDF$$2rda
000838618 4901_ $$aSpringer aerospace technology,$$x1869-1730
000838618 504__ $$aIncludes bibliographical references and index.
000838618 5050_ $$aIntro; Preface; Acknowledgements; Contents; List of Figures; List of Tables; List of Programs; 1 Introduction; 1.1 Preliminary; 1.2 Book Highlights; 1.3 Chapters' Organization; 2 Flight Mechanics; 2.1 Basic Flight System; 2.2 Steady Straight Level Flight; 2.3 Takeoff Maneuver; 2.4 Glider Design; 2.5 Aircraft Failures; 3 Navigational Modules; 3.1 Magnetic Heading Sensing; 3.2 Acceleration Sensor; 3.3 Global Positioning System; 3.3.1 GPS Experiment; 3.4 Integrated Navigational System; 4 Flight Simulator Systems; 4.1 Flight Software and Yoke; 4.2 Aircraft C-130 Simulator
000838618 5058_ $$a4.3 Flight Determination of Aircraft Performance4.4 Experimental Setup; 5 Tandem Rotor Helicopter Control; 5.1 Fundamentals of Control System; 5.2 Tandem Rotor Modelling; 5.3 PID Control Scheme; 5.4 Elevation Control Analysis; 5.4.1 Elevation Control; 5.4.2 Elevation Controllers Design; 5.5 Elevation Disturbance Control; 5.6 Pitch Control Analysis; 5.6.1 Pitch Control; 5.6.2 Pitch Controllers Design; 5.7 Travel Control Analysis; 5.7.1 Travel Position Control; 5.7.2 Travel Position Controller Design; 5.8 Travel Rate Control Analysis; 5.8.1 Travel Rate Control
000838618 5058_ $$a5.8.2 Travel Rate Controller Design5.9 3-DOF Helicopter Control System; 5.10 Real Time Control Implementation; 6 Unmanned Aerial Vehicle System; 6.1 Autopilots; 6.2 Machine Vision Payload; 6.3 Telemetry; 6.4 Ground Control Station; 6.5 Unmanned Wooden Airplane; 7 Rotorcrafts; 7.1 Quadrotor Modelling; 7.1.1 Hovering Body Parallel to the Ground; 7.1.2 Altitude Control; 7.2 State-Space Control Method; 7.3 Attitude LQR Controller; 7.4 Attitude Control Result; 7.5 Control of the Quadcopter; 7.6 LQR Control Technique; 7.6.1 Controllability and Observability; 7.6.2 Modified LQR Control
000838618 5058_ $$a7.6.3 The Threshold Value7.7 Quadcopter Computations; 7.8 Multiple Quadcopters; 8 Flight Instrumentation Acquisition; 8.1 Inertial Navigation Systems; 8.2 INS Hardware Interface; 8.3 Sensor Information Acquisition; 8.4 GUI Software Development; 8.4.1 Internal Computation; 8.4.2 Main Function Block; 8.4.3 Input Configuration; 8.5 Robotic Navigational Sensor; 8.5.1 Packet Signals; 8.5.2 GPS Receiving Signal; 8.6 IMU Data Extraction; 8.7 IMU 3D Model Acquisition; 8.7.1 VRML Model; 8.7.2 IMU Model Attitude Control; 9 Recent and Future Developments; 9.1 Solar UAV; 9.1.1 Solar-Powered Methodology
000838618 5058_ $$a9.1.2 Wind Tunnel Model9.1.3 Flight System; 9.1.4 Long Endurance UAV Flight; 9.2 Wind-Powered Energy Source; 9.3 Fuel Cell Technology; 9.4 Vertical Takeoff/Landing Air Vehicles; 9.5 New Stealth Technology; 9.6 Aerial Systems Improvements; Appendix A: LabVIEW Functions; Appendix B: Tricopter Graphical Programming; Appendix C: Questions; References; Index
000838618 506__ $$aAccess limited to authorized users.
000838618 520__ $$aThis book focuses on flight vehicles and their navigational systems, discussing different forms of flight structures and their control systems, from fixed wings to rotary crafts. Software simulation enables testing of the hardware without actual implementation, and the flight simulators, mechanics, glider development and navigation systems presented here are suitable for lab-based experimentation studies. It explores laboratory testing of flight navigational sensors, such as the magnetic, acceleration and Global Positioning System (GPS) units, and illustrates the six-axis inertial measurement unit (IMU) instrumentation as well as its data acquisition methodology. The book offers an introduction to the various unmanned aerial vehicle (UAV) systems and their accessories, including the linear quadratic regulator (LQR) method for controlling the rotorcraft. It also describes a Matrix Laboratory (MATLAB) control algorithm that simulates and runs the lab- based 3 degrees of freedom (DOF) helicopter, as well as LabVIEW software used to validate controller design and data acquisition. Lastly, the book explores future developments in aviation techniques.
000838618 588__ $$aOnline resource; title from PDF title page (SpringerLink, viewed April 16, 2018).
000838618 650_0 $$aFlight control.
000838618 77608 $$iPrint version: $$z9811087202$$z9789811087202$$w(OCoLC)1022781954
000838618 830_0 $$aSpringer aerospace technology.
000838618 852__ $$bebk
000838618 85640 $$3SpringerLink$$uhttps://univsouthin.idm.oclc.org/login?url=http://link.springer.com/10.1007/978-981-10-8721-9$$zOnline Access$$91397441.1
000838618 909CO $$ooai:library.usi.edu:838618$$pGLOBAL_SET
000838618 980__ $$aEBOOK
000838618 980__ $$aBIB
000838618 982__ $$aEbook
000838618 983__ $$aOnline
000838618 994__ $$a92$$bISE