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Flight Systems and Control -  Tian Seng Ng

Flight Systems and Control (eBook)

A Practical Approach

(Autor)

eBook Download: PDF
2018 | 1. Auflage
XXIII, 254 Seiten
Springer Singapore (Verlag)
978-981-10-8721-9 (ISBN)
Systemvoraussetzungen
117,69 inkl. MwSt
(CHF 114,95)
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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.



Mr Tian Seng Ng has an MSc degree in Computer Control and Automation. He is a member of the technical staff at the Nanyang Technological University. He has been active in the field of         robotics, control and automation for almost 25 year, and has worked on gantry crane automation systems at wharves and field pumping stations in Singapore. His interest lies in the domain of   instrumentation, mechatronics, control systems and machine vision.

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.

Mr. Tian Seng Ng has a MSc degree in Computer Control and Automation. He is a member of the technical staff at the Nanyang Technological University. He has been active in the field of flight robotics, control, and automation for almost 25 years, and has worked on gantry crane automation systems at wharves and field pumping stations in Singapore. His interest lies in the domain of control, mechatronics, autonomous systems and machine vision.

Preface 7
Acknowledgements 9
Contents 10
List of Figures 13
List of Tables 18
List of Programs 19
1 Introduction 20
1.1 Preliminary 20
1.2 Book Highlights 20
1.3 Chapters’ Organization 21
2 Flight Mechanics 22
2.1 Basic Flight System 22
2.2 Steady Straight Level Flight 22
2.3 Takeoff Maneuver 27
2.4 Glider Design 28
2.5 Aircraft Failures 28
3 Navigational Modules 31
3.1 Magnetic Heading Sensing 31
3.2 Acceleration Sensor 38
3.3 Global Positioning System 44
3.3.1 GPS Experiment 51
3.4 Integrated Navigational System 58
4 Flight Simulator Systems 60
4.1 Flight Software and Yoke 60
4.2 Aircraft C-130 Simulator 63
4.3 Flight Determination of Aircraft Performance 65
4.4 Experimental Setup 69
5 Tandem Rotor Helicopter Control 71
5.1 Fundamentals of Control System 71
5.2 Tandem Rotor Modelling 75
5.3 PID Control Scheme 79
5.4 Elevation Control Analysis 81
5.4.1 Elevation Control 81
5.4.2 Elevation Controllers Design 93
5.5 Elevation Disturbance Control 98
5.6 Pitch Control Analysis 102
5.6.1 Pitch Control 102
5.6.2 Pitch Controllers Design 103
5.7 Travel Control Analysis 104
5.7.1 Travel Position Control 104
5.7.2 Travel Position Controller Design 105
5.8 Travel Rate Control Analysis 107
5.8.1 Travel Rate Control 107
5.8.2 Travel Rate Controller Design 108
5.9 3-DOF Helicopter Control System 111
5.10 Real Time Control Implementation 114
6 Unmanned Aerial Vehicle System 124
6.1 Autopilots 124
6.2 Machine Vision Payload 126
6.3 Telemetry 129
6.4 Ground Control Station 131
6.5 Unmanned Wooden Airplane 132
7 Rotorcrafts 134
7.1 Quadrotor Modelling 134
7.1.1 Hovering Body Parallel to the Ground 134
7.1.2 Altitude Control 136
7.2 State-Space Control Method 136
7.3 Attitude LQR Controller 140
7.4 Attitude Control Result 141
7.5 Control of the Quadcopter 142
7.6 LQR Control Technique 145
7.6.1 Controllability and Observability 145
7.6.2 Modified LQR Control 148
7.6.3 The Threshold Value 151
7.7 Quadcopter Computations 153
7.8 Multiple Quadcopters 162
8 Flight Instrumentation Acquisition 169
8.1 Inertial Navigation Systems 169
8.2 INS Hardware Interface 170
8.3 Sensor Information Acquisition 171
8.4 GUI Software Development 176
8.4.1 Internal Computation 176
8.4.2 Main Function Block 176
8.4.3 Input Configuration 179
8.5 Robotic Navigational Sensor 182
8.5.1 Packet Signals 186
8.5.2 GPS Receiving Signal 189
8.6 IMU Data Extraction 197
8.7 IMU 3D Model Acquisition 204
8.7.1 VRML Model 204
8.7.2 IMU Model Attitude Control 207
9 Recent and Future Developments 213
9.1 Solar UAV 213
9.1.1 Solar-Powered Methodology 214
9.1.2 Wind Tunnel Model 215
9.1.3 Flight System 216
9.1.4 Long Endurance UAV Flight 217
9.2 Wind-Powered Energy Source 217
9.3 Fuel Cell Technology 219
9.4 Vertical Takeoff/Landing Air Vehicles 221
9.5 New Stealth Technology 224
9.6 Aerial Systems Improvements 225
10 Erratum to: Flight Systems and Control 226
Erratum to:& #6
Appendix A: LabVIEW Functions 227
Appendix B: Tricopter Graphical Programming 241
Appendix C: Questions 245
References 251
Index 252

Erscheint lt. Verlag 13.4.2018
Reihe/Serie Springer Aerospace Technology
Zusatzinfo XXV, 241 p. 206 illus., 163 illus. in color.
Verlagsort Singapore
Sprache englisch
Themenwelt Informatik Theorie / Studium Algorithmen
Informatik Theorie / Studium Künstliche Intelligenz / Robotik
Technik Elektrotechnik / Energietechnik
Technik Fahrzeugbau / Schiffbau
Technik Luft- / Raumfahrttechnik
Schlagworte Aircraft C-130 Simulator • Aircraft Failures • Flight Instrumentation Acquisition • Glider Design • Machine Vision Payload • Magnetic Heading Sensing • Quadcopter Computations • Real Time Control Implementation • Robotic Navigational Sensor • Rotorcrafts • Tandem Rotor Helicopter Control • unmanned aerial vehicles (UAV) • Unmanned Wooden Airplane • Vertical Takeoff/Landing Air Vehicles
ISBN-10 981-10-8721-0 / 9811087210
ISBN-13 978-981-10-8721-9 / 9789811087219
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