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      Design of unmanned aerial systems

      한글로보기

      https://www.riss.kr/link?id=M15590752

      • 저자
      • 발행사항

        Hoboken, NJ : John Wiley & Sons, 2019

      • 발행연도

        2019

      • 작성언어

        영어

      • 주제어
      • DDC

        629.13339 판사항(23)

      • ISBN

        9781119508700 (hardback)

      • 자료형태

        단행본(다권본)

      • 발행국(도시)

        New Jersey

      • 서명/저자사항

        Design of unmanned aerial systems / Dr. Mohammad H. Sadraey.

      • 형태사항

        xxxvii, 623 p. : ill. ; 25 cm.

      • 총서사항

        Aerospace series

      • 일반주기명

        Includes bibliographical references and index.

      • 소장기관
        • 국립중앙도서관 국립중앙도서관 우편복사 서비스
        • 서강대학교 도서관 소장기관정보 Deep Link
        • 중앙대학교 서울캠퍼스 학술정보원 소장기관정보 Deep Link
        • 한국과학기술원(KAIST) 학술문화관 소장기관정보
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      목차 (Table of Contents)

      • CONTENTS
      • Preface = xix
      • Acronyms = xxv
      • Nomenclature = xxix
      • About the Companion Website = xxxvii
      • CONTENTS
      • Preface = xix
      • Acronyms = xxv
      • Nomenclature = xxix
      • About the Companion Website = xxxvii
      • 1 Design Fundamentals = 1
      • 1.1 Introduction = 2
      • 1.2 UAV Classifications = 5
      • 1.3 Review of a Few Successful UAVs = 8
      • 1.3.1 Global Hawk = 8
      • 1.3.2 RQ-1A Predator = 9
      • 1.3.3 MQ-9 Predator B Reaper = 9
      • 1.3.4 RQ-5A Hunter = 10
      • 1.3.5 RQ-7 Shadow 200 = 10
      • 1.3.6 RQ-2A Pioneer = 11
      • 1.3.7 RQ-170 Sentinel = 11
      • 1.3.8 X-45A UCAV = 12
      • 1.3.9 Epson Micro-flying Robot = 12
      • 1.4 Design Project Planning = 12
      • 1.5 Decision Making = 13
      • 1.6 Design Criteria, Objectives, and Priorities = 15
      • 1.7 Feasibility Analysis = 17
      • 1.8 Design Groups = 17
      • 1.9 Design Process = 18
      • 1.10 Systems Engineering Approach = 19
      • 1.11 UAV Conceptual Design = 21
      • 1.12 UAV Preliminary Design = 27
      • 1.13 UAV Detail Design = 28
      • 1.14 Design Review, Evaluation, Feedback = 30
      • 1.15 UAV Design Steps = 30
      • Questions = 32
      • 2 Preliminary Design = 35
      • 2.1 Introduction = 35
      • 2.2 Maximum Takeoff Weight Estimation = 36
      • 2.3 Weight Buildup = 36
      • 2.4 Payload Weight = 37
      • 2.5 Autopilot Weight = 37
      • 2.6 Fuel Weight = 39
      • 2.7 Battery Weight = 43
      • 2.8 Empty Weight = 47
      • 2.9 Wing and Engine Sizing = 48
      • 2.10 Quadcopter Configuration = 52
      • Questions = 60
      • Problems = 61
      • 3 Design Disciplines = 65
      • 3.1 Introduction = 66
      • 3.2 Aerodynamic Design = 67
      • 3.3 Structural Design = 69
      • 3.4 Propulsion System Design = 71
      • 3.4.1 General Design Guidelines = 72
      • 3.4.2 Electric Engines = 74
      • 3.5 Landing Gear Design = 75
      • 3.6 Mechanical and Power Transmission Systems Design = 78
      • 3.7 Electric Systems = 80
      • 3.7.1 Fundamentals = 80
      • 3.7.2 Safety Recommendations = 81
      • 3.7.3 Wiring Diagrams = 82
      • 3.7.4 Wire Insulation and Shielding = 83
      • 3.7.5 Batteries = 83
      • 3.7.6 Generator = 84
      • 3.8 Control Surfaces Design = 85
      • 3.9 Safety Analysis = 90
      • 3.9.1 Design Lessons Learned = 91
      • 3.9.2 Likely Failure Modes of Sub-Systems Componets = 93
      • 3.10 Installation Guidelines = 95
      • 3.10.1 GPS/Compass = 95
      • 3.10.2 IMU = 95
      • 3.10.3 Electric Motor = 96
      • Questions = 96
      • Design Questions = 97
      • Problems = 99
      • 4 Aerodynamic Design = 101
      • 4.1 Introduction = 102
      • 4.2 Fundamentals of Aerodynamics = 103
      • 4.3 Wing Design = 104
      • 4.3.1 Wing Design Procedure = 105
      • 4.3.2 Airfoil Selection/Design = 106
      • 4.3.3 Wing Design Technique = 108
      • 4.3.4 Wing Design Steps = 113
      • 4.4 Tail Design = 113
      • 4.4.1 Design Procedure = 113
      • 4.4.2 Tail Configuration = 115
      • 4.4.3 Horizontal Tail Design Technique = 116
      • 4.4.4 Tail Planform Area and Tail Arm = 117
      • 4.4.5 Tail Airfoil Section = 118
      • 4.4.6 Tail Incidence = 119
      • 4.4.7 Other Horizontal Tail Parameters = 119
      • 4.5 Vertical Tail Design = 119
      • 4.5.1 Parameters = 119
      • 4.5.2 Vertical Tail Location = 120
      • 4.5.3 Vertical Tai Moment Arm (lvt) = 120
      • 4.5.4 Planform Area (Sv) = 120
      • 4.5.5 Incidence (iv) = 121
      • 4.5.6 Other Vertical Tail Paramenters = 122
      • 4.5.7 Vertical Tail Design Technique = 122
      • 4.6 Fuselage Design = 123
      • 4.6.1 Fuselage Design Fundamentals = 123
      • 4.6.2 Fuselage Aerodynamics = 123
      • 4.6.3 Autopilot Compartment = 126
      • 4.6.4 Optimum Length-to-Diameter Ratio = 126
      • 4.6.5 Fuselage Aerodynamics = 127
      • 4.6.6 Lofting = 128
      • 4.6.7 Fuselage Design Steps = 129
      • 4.7 Antenna = 130
      • 4.7.1 Fixed Antenna = 130
      • 4.7.2 Radar Dish Antenna = 131
      • 4.7.3 Satellite Communication Antenna = 131
      • 4.7.4 Antenna Design/Installation = 132
      • 4.8 Aerodynamic Design of Quadcopters = 132
      • 4.9 Aerodynamic Design Guidelines = 133
      • Questions = 134
      • Problems = 136
      • 5 Fundamentals of Autopilot Design = 141
      • 5.1 Introduction = 142
      • 5.1.1 Autopilot and Human Operator = 143
      • 5.1.2 Primary Subsystems of an Autopilot = 144
      • 5.1.3 Autopilot Design or Selection = 145
      • 5.2 Dynamic Modeling = 146
      • 5.2.1 Modeling Technique = 146
      • 5.2.2 Fundamental Model = 148
      • 5.2.3 Transfer Function = 150
      • 5.2.4 State-Space Representation = 152
      • 5.3 Aerodynamic Forces and Moments = 153
      • 5.3.1 Forces and Moments Equations = 153
      • 5.3.2 Stability and Control Derivatives = 154
      • 5.3.3 Non-kdimensional Stability and Control Derivatives = 154
      • 5.3.4 Dimensional Stability and Control Derivatives = 155
      • 5.3.5 Coupling Stability Derivatives = 156
      • 5.4 Simplification Techniques of Dynamic Models = 157
      • 5.4.1 Linearization = 157
      • 5.4.2 Decoupling = 159
      • 5.5 Fixed-Wing UAV Dynamic Models = 161
      • 5.5.1 Nonlinear Fully Coupled Equations of Motion = 162
      • 5.5.2 Nonlinear Semi-Coupled Equations of Motion = 162
      • 5.5.3 Nonlinear Decoupled Equations of Motion = 163
      • 5.5.4 Linear Coupled Equations of Motion = 163
      • 5.5.5 Linear Decoupled Equations of Motion = 165
      • 5.5.6 Reformulated (Nonlinear Semi-Coupled) Equations of Motion = 167
      • 5.5.7 Un-powered Gliding Equations of Motion = 168
      • 5.6 Dynamic Model Approximation = 169
      • 5.6.1 Pure Pitching Motion Approximation = 169
      • 5.6.2 Pure Rolling Motion Approximation = 169
      • 5.6.3 Pure Yawing Motion Approximation = 169
      • 5.6.4 Longitudinal Oscillatory Modes Approximation = 170
      • 5.7 Quadcopter (Rotary-Wing) Dynamic Model = 170
      • 5.7.1 Overall Thrust of Four Motors = 170
      • 5.7.2 Dynamic Model = 174
      • 5.7.3 Simplified Dynamic Model = 175
      • 5.8 Autopilot Categories = 176
      • 5.8.1 Stability Augmentation = 176
      • 5.8.2 Hold Functions = 178
      • 5.8.3 Navigation Functions = 180
      • 5.8.4 Command Augmentation Systems = 180
      • 5.9 Flight Simulation - Numerical Methods = 181
      • 5.9.1 Numerical Integration = 182
      • 5.9.2 Matlab/Simulink = 182
      • 5.9.3 Hardware-In-the-Loop Simulation = 184
      • 5.10 Flying Qualities for UAVs = 185
      • 5.10.1 Fundamentals = 185
      • 5.10.2 Classes, Categories, and Acceptability Levels = 186
      • 5.10.3 Force Restrietions = 186
      • 5.11 Autopilot Design Process = 187
      • Questions = 188
      • Problems = 190
      • 6 Control System Design = 195
      • 6.1 Introduction = 196
      • 6.2 Fundamentals of Control Systems = 197
      • 6.2.1 Elements, Concepts and Definitions = 197
      • 6.2.2 Root Locus Design Technique = 199
      • 6.2.3 Frequency Domain Design Technique = 200
      • 6.2.4 Controller Configurations and Control Architectures = 201
      • 6.3 Servo/Actuator = 203
      • 6.3.1 Terminology = 203
      • 6.3.2 Electric Motors = 204
      • 6.3.3 Hydraulic Actuator = 206
      • 6.3.4 Delay = 206
      • 6.3.5 Saturation = 207
      • 6.4 Flight Control Requirements = 207
      • 6.4.1 Longitudinal Control Requirements = 207
      • 6.4.2 Roll Control Requirements = 208
      • 6.4.3 Directional Control Requirements = 209
      • 6.5 Control Modes = 209
      • 6.5.1 Coupled Control Modes = 210
      • 6.5.2 Cruise Control = 212
      • 6.5.3 Pitch-Attitude Hold = 213
      • 6.5.4 Wing Leveler = 214
      • 6.5.5 Yaw Damper = 215
      • 6.5.6 Auto-Landing = 217
      • 6.5.7 Turn Coordinator = 218
      • 6.6 Controller Design = 223
      • 6.6.1 PID Controller = 223
      • 6.6.2 Optimal Control - LQR = 224
      • 6.6.3 Gain Scheduling = 229
      • 6.6.4 Robust Control = 231
      • 6.6.5 Digital Control = 233
      • 6.7 Autonomy = 234
      • 6.7.1 Classification = 234
      • 6.7.2 Detect (i.e., Sense)-and-Avoid = 235
      • 6.7.3 Automated Recovery = 236
      • 6.7.4 Fault Monitoring = 236
      • 6.7.5 Intelligent Flight Planning = 236
      • 6.8 Manned-Unmanned Aircraft Teaming = 237
      • 6.8.1 Need for Teaming = 237
      • 6.8.2 Teaming Problem Formulation = 237
      • 6.8.3 Decision Making Process = 239
      • 6.8.4 Teaming Communication Process = 241
      • 6.8.5 Teaming Laws = 242
      • 6.9 Control System Design Process = 243
      • Questions = 246
      • Problems = 249
      • 7 Guidance System Design = 255
      • 7.1 Introduction = 256
      • 7.2 Fundamentals = 257
      • 7.2.1 Guidance Process = 257
      • 7.2.2 Elements of Guidance System = 258
      • 7.2.3 Guidance Components = 259
      • 7.2.4 Target Detection = 260
      • 7.2.5 Moving Target Tracking = 262
      • 7.3 Guidance Laws = 263
      • 7.4 Command Guidance Law = 265
      • 7.5 PN Guidance Law = 269
      • 7.6 Pursuit Guidance Law = 273
      • 7.7 Waypoint Guidance Law = 274
      • 7.7.1 Waypoints = 274
      • 7.7.2 Types of Waypoint Guidance = 275
      • 7.7.3 Segments of a Horizontal (Level) Trajectory = 276
      • 7.7.4 Waypoint Guidance Algorithm = 278
      • 7.7.5 UAV Maneuverability Evaluation = 281
      • 7.8 Sense and Avoid = 282
      • 7.8.1 Fundamentals = 282
      • 7.8.2 Sensing Techniques = 283
      • 7.8.3 Collision Avoidance = 286
      • 7.9 Formation Flight = 291
      • 7.10 Motion Planning and Trajectory Design = 293
      • 7.11 Guidance Sensor - Seeker = 294
      • 7.12 Guidance System Design = 296
      • Questions = 298
      • Problems = 300
      • 8 Navigation System Design = 305
      • 8.1 Introduction = 306
      • 8.2 Classifications = 307
      • 8.3 Coordinate Systems = 309
      • 8.3.1 Fixed and Moving Frames = 309
      • 8.3.2 World Geodetic System = 310
      • 8.4 Inertial Navigation System = 311
      • 8.4.1 Fundamentals = 311
      • 8.4.2 Navigation Equations = 313
      • 8.4.3 Navigation Basic Calculations = 313
      • 8.4.4 Geodetic Coordinates Calculations = 314
      • 8.5 Kalman Filtering = 315
      • 8.6 Global Positioning System = 317
      • 8.6.1 Fundamentals = 317
      • 8.6.2 Earth Longitude and Latitude = 319
      • 8.6.3 Ground Speed Versus Airspeed = 322
      • 8.7 Position Fixing Navigation = 322
      • 8.7.1 Map Reading = 322
      • 8.7.2 Celestial Navigation = 322
      • 8.8 Navigation in Reduced Visibility Conditions = 323
      • 8.9 Inertial Navigation Sensors = 323
      • 8.9.1 Primary Functions = 323
      • 8.9.2 Accelerometer = 324
      • 8.9.3 Gyroscope = 326
      • 8.9.4 Airspeed Sensor = 329
      • 8.9.5 Altitude Sensor = 330
      • 8.9.6 Pressure Sensor = 332
      • 8.9.7 Clock/Time = 332
      • 8.9.8 Compass = 332
      • 8.9.9 Magnetometer = 333
      • 8.9.10 MEMS Inertial Module = 333
      • 8.9.11 Transponder = 335
      • 8.10 Navigation Disturbances = 335
      • 8.10.1 Wind = 335
      • 8.10.2 Gust and Disturbance = 337
      • 8.10.3 Measurement Noise = 339
      • 8.10.4 Drift = 340
      • 8.10.5 Coriolis Effect = 342
      • 8.10.6 Magnetic Deviation = 344
      • 8.11 Navigation System Design = 345
      • 8.11.1 Design Requirements = 345
      • 8.11.2 Design Flowchart = 346
      • 8.11.3 Design Guidelines = 347
      • Questions = 348
      • Problems = 352
      • 9 Microcontroller = 355
      • 9.1 Introduction = 356
      • 9.2 Basic Fundamentals = 358
      • 9.2.1 Microcontroller Basics = 358
      • 9.2.2 Microcontroller Versus Microprocessor = 361
      • 9.2.3 Packaging Formats = 361
      • 9.2.4 Modules/Components = 363
      • 9.2.5 Atmel ATmega644P = 365
      • 9.3 Microcontroller Circuitry = 367
      • 9.3.1 Microcontroller Circuit Board = 367
      • 9.3.2 Electric Motor = 367
      • 9.3.3 Servo Motor = 368
      • 9.3.4 Sensors = 368
      • 9.3.5 Potentiometer = 369
      • 9.4 Embedded Systems = 369
      • 9.4.1 Introduction = 369
      • 9.4.2 Embedded Processors = 369
      • 9.4.3 Signal Flow = 370
      • 9.5 Microcontroller Programming = 371
      • 9.5.1 Software Development = 371
      • 9.5.2 Operating System = 371
      • 9.5.3 Management Software = 371
      • 9.5.4 Microcontroller Programing = 372
      • 9.5.5 Software Integration = 372
      • 9.5.6 High-Level Programming Languages = 373
      • 9.5.7 Compiler = 374
      • 9.5.8 Debugging = 374
      • 9.6 Programming in C = 374
      • 9.6.1 Introduction = 374
      • 9.6.2 General Structure of a C Program = 374
      • 9.6.3 Example Code - Detecting a Dead LED = 375
      • 9.6.4 Execution of a C Program = 377
      • 9.7 Arduino = 378
      • 9.7.1 Arduino Overview = 378
      • 9.7.2 Arduino Programming = 379
      • 9.7.3 Arduino Uno Board = 380
      • 9.7.4 Open-Loop Control of an Elevator = 382
      • 9.7.5 Arduino and Matlab = 383
      • 9.8 Open-Source Commercial Autopilots = 384
      • 9.8.1 ArduPilot = 384
      • 9.8.2 PX4 Pixhawk Autopilot = 385
      • 9.8.3 Micropilot = 386
      • 9.8.4 DJI WookKong Autopilot = 387
      • 9.9 Design Procedure = 387
      • 9.10 Design Project = 388
      • 9.10.1 Problem Statement = 389
      • 9.10.2 Design and Implementation = 389
      • 9.10.3 Arduino Code = 389
      • 9.10.4 Procedure = 391
      • 9.10.5 MATLAB Code for Real-Time Plotting = 392
      • 9.10.6 System Response and Results = 393
      • Questions = 393
      • Problems = 395
      • Design Projects = 397
      • 10 Launch and Recovery Systems Design = 399
      • 10.1 Introduction = 400
      • 10.2 Launch Technologies and Techniques = 402
      • 10.2.1 Rocket Assisted Launch = 402
      • 10.2.2 Bungee Cord Catapult Launch = 403
      • 10.2.3 Pneumatic Launchers = 406
      • 10.2.4 Hydraulic Launchers = 407
      • 10.2.5 Air Launch = 408
      • 10.2.6 Hand Launch = 409
      • 10.3 Launcher Equipment = 410
      • 10.3.1 Elements = 410
      • 10.3.2 Ramp/Slipway = 410
      • 10.3.3 Push Mechanism = 412
      • 10.3.4 Elevation Platform = 412
      • 10.3.5 Power Supply = 415
      • 10.4 Fundamentals of Launch = 415
      • 10.4.1 Fundamental Principles = 415
      • 10.4.2 Governing Launch Equations = 416
      • 10.4.3 Wing and Horizontal Tail Contributions = 419
      • 10.4.4 UAV Longitudinal Trim = 420
      • 10.5 Elevation Mechanism Design = 422
      • 10.5.1 Elevation Mechanism Operation = 422
      • 10.5.2 Hydraulic and Pneumatic Actuators = 423
      • 10.6 VTOL = 424
      • 10.7 Recovery Technologies and Techniques = 424
      • 10.7.1 Fundamentals = 424
      • 10.7.2 Net Recovery = 425
      • 10.7.3 Arresting Line = 426
      • 10.7.4 Skyhook = 427
      • 10.7.5 Windsock = 427
      • 10.7.6 Parachute = 429
      • 10.8 Recovery Fundamentals = 429
      • 10.8.1 Parachute = 429
      • 10.8.2 Impact Recovery = 431
      • 10.9 Launch/Recovery Systems Mobility = 431
      • 10.9.1 Mobility Requirements = 431
      • 10.9.2 Conventional Wheeled Vehicle = 432
      • 10.10 Launch and Recovery Systems Design = 433
      • 10.10.1 Launch and Recovery Techniques Selection = 433
      • 10.10.2 Launch System Design = 434
      • 10.10.3 Recovery System Design = 436
      • Questions = 437
      • Problems = 440
      • Design Projects = 443
      • 11 Ground Control Station = 445
      • 11.1 Introduction = 446
      • 11.2 GCS Subsystems = 448
      • 11.3 Types of Ground Stations = 448
      • 11.3.1 Handheld Radio Controller = 449
      • 11.3.2 Portable GCS = 453
      • 11.3.3 Mobile Truck = 454
      • 11.3.4 Central Command Station = 458
      • 11.3.5 Sea Control Station = 459
      • 11.3.6 General GCS = 459
      • 11.4 GCS of a Number of UAVs = 460
      • 11.4.1 Global Hawk = 460
      • 11.4.2 Predator = 461
      • 11.4.3 MQ-5A Hunter = 462
      • 11.4.4 Shadow 200 = 462
      • 11.4.5 DJI Phantom = 463
      • 11.4.6 Yamaha RMAX Unmanned Helicopter = 464
      • 11.5 Human-Related Design Requirements = 464
      • 11.5.1 Number of Pilots Operators in Ground Station = 464
      • 11.5.2 Ergonomics = 464
      • 11.5.3 Features of a Human Pilot/Operator = 466
      • 11.5.4 Console Dimensions and Limits = 467
      • 11.6 Support Equipment = 469
      • 11.6.1 Introduction = 469
      • 11.6.2 Transportation Equipment = 470
      • 11.6.3 Power Generator = 471
      • 11.6.4 HVAC System = 471
      • 11.6.5 Other Items = 471
      • 11.7 GCS Design Guidelines = 472
      • Questions = 473
      • Problems = 475
      • Design Problems = 476
      • Laboratory Experiments = 477
      • 12 Payloads Selection/Design = 487
      • 12.1 Introduction = 482
      • 12.2 Elements of Payload = 483
      • 12.2.1 Payload Definition = 483
      • 12.2.2 Payloads Classifications = 484
      • 12.3 Payloads of a Few UAVs = 484
      • 12.3.1 RQ-4 Global Hawk = 485
      • 12.3.2 MQ-9 Predator B Reaper = 485
      • 12.3.3 RQ-7 Shadow 200 = 486
      • 12.3.4 RQ-5A Hunter = 486
      • 12.3.5 DJI Phantom Quadcopter = 486
      • 12.3.6 X-45 UCAV = 487
      • 12.3.7 Yamaha RMAX = 487
      • 12.4 Cargo or Freight Payload = 487
      • 12.5 Reconnaissance/Surveillance Payload = 488
      • 12.5.1 Electro-Optical Camera = 489
      • 12.5.2 Infra-Red Camera = 494
      • 12.5.3 Radar = 495
      • 12.5.4 Lidar = 502
      • 12.5.5 Range Finder = 502
      • 12.5.6 Laser Designator = 504
      • 12.5.7 Radar Warning Receiver = 505
      • 12.6 Scientific Payloads = 505
      • 12.6.1 Classifications = 505
      • 12.6.2 Temperature Sensor = 507
      • 12.7 Military Payloads = 508
      • 12.8 Electronic Counter Measure Payloads = 509
      • 12.9 Payload Installation = 511
      • 12.9.1 Payload Wiring = 511
      • 12.9.2 Payload Location = 512
      • 12.9.3 Payload Aerodynamics = 513
      • 12.9.4 Payload-Structure Integration = 517
      • 12.9.5 Payload Stabilization = 520
      • 12.10 Payload Control and Management = 520
      • 12.11 Payload Selection/Design Guidelines = 520
      • Questions = 523
      • Problems = 525
      • Design Problems = 527
      • 13 Communications System Design = 531
      • 13.1 Fundamentals = 532
      • 13.2 Data Link = 534
      • 13.3 Transmitter = 536
      • 13.4 Receiver = 537
      • 13.5 Antenna = 539
      • 13.6 Radio Frequency = 541
      • 13.7 Encryption = 544
      • 13.8 Communications Systems of a Few UAVs = 545
      • 13.9 Installation = 547
      • 13.10 Communications System Design = 547
      • 13.11 Bi-directional Communications Using Arduino Boards = 548
      • 13.11.1 Communications Modules = 548
      • 13.11.2 NRF24L01 Module = 549
      • 13.11.3 Bluetooth Module = 553
      • 13.11.4 An Application = 554
      • Questions = 558
      • Problems = 560
      • Laboratory Experiments = 561
      • Design Projects = 562
      • 14 Design Analysis and Feedbacks = 565
      • 14.1 Introduction = 566
      • 14.2 Design Feedbacks = 567
      • 14.3 Weight and Balance = 569
      • 14.3.1 UAV Center of Gravity = 569
      • 14.3.2 Weight Distribution = 471
      • 14.4 Stability Analysis = 573
      • 14.4.1 Fundamentals = 573
      • 14.4.2 Static Longitudinal Stability = 574
      • 14.4.3 Dynamic Longitudinal Stability = 574
      • 14.4.4 Static Lateral-Directional Stability = 575
      • 14.4.5 Dynamic Lateral-Directional Stability = 576
      • 14.4.6 Typical Values for Stability Derivatives = 577
      • 14.5 Controllability Analysis = 579
      • 14.5.1 Longitudinal Control = 579
      • 14.5.2 Lateral Control = 580
      • 14.5.3 Directional Control = 581
      • 14.5.4 Typical Values for Control Derivatives = 582
      • 14.6 Flight Performance Analysis = 582
      • 14.6.1 Maximum Speed = 582
      • 14.6.2 Maximum Range = 584
      • 14.6.3 Maximum Endurance = 584
      • 14.6.4 Climb Performance = 585
      • 14.6.5 Takeoff Performance = 587
      • 14.6.6 Turn Performance = 588
      • 14.6.7 Absolute Ceiling = 590
      • 14.7 Cost Analysis = 591
      • Questions = 593
      • Problems = 595
      • References = 601
      • Index = 609
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      Design of Unmanned Aerial Systems

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