Merkzettel Warenkorb
Produktbild: Aircraft Control and Simulation

Aircraft Control and Simulation Dynamics, Controls Design, and Autonomous Systems

192,99 €

inkl. gesetzl. MwSt., Versandkostenfrei

Lieferung nach Hause

Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

02.11.2015

Verlag

John Wiley & Sons

Seitenzahl

768

Maße (L/B/H)

24,1/15,8/4,5 cm

Gewicht

1191 g

Auflage

3rd Revised edition

Sprache

Englisch

ISBN

978-1-118-87098-3

Beschreibung

Produktdetails

Einband

Gebundene Ausgabe

Erscheinungsdatum

02.11.2015

Verlag

John Wiley & Sons

Seitenzahl

768

Maße (L/B/H)

24,1/15,8/4,5 cm

Gewicht

1191 g

Auflage

3rd Revised edition

Sprache

Englisch

ISBN

978-1-118-87098-3

Herstelleradresse

Libri GmbH
Europaallee 1
36244 Bad Hersfeld
DE

Email: GPSR Kontakt

Noch keine Bewertungen vorhanden

Verfassen Sie die erste Bewertung zu diesem Artikel

Helfen Sie anderen Kundinnen und Kunden durch Ihre Meinung.

Kundinnen und Kunden meinen

Bewertungen (0)
Die Leseprobe wird geladen.
  • Produktbild: Aircraft Control and Simulation

  • Preface xi

    1 The Kinematics and Dynamics of Aircraft Motion 1

    1.1 Introduction 1

    1.2 Vector Operations 3

    1.3 Matrix Operations on Vector Coordinates 7

    1.4 Rotational Kinematics 16

    1.5 Translational Kinematics 20

    1.6 Geodesy, Coordinate Systems, Gravity 23

    1.7 Rigid-Body Dynamics 34

    1.8 Advanced Topics 44

    References 58

    Problems 59

    2 Modeling the Aircraft 63

    2.1 Introduction 63

    2.2 Basic Aerodynamics 64

    2.3 Aircraft Forces And Moments 75

    2.4 Static Analysis 101

    2.5 The Nonlinear Aircraft Model 108

    2.6 Linear Models And The Stability Derivatives 116

    2.7 Summary 137

    References 138

    Problems 139

    3 Modeling, Design, and Simulation Tools 142

    3.1 Introduction 142

    3.2 State-Space Models 144

    3.3 Transfer Function Models 155

    3.4 Numerical Solution of The State Equations 170

    3.5 Aircraft Models For Simulation 179

    3.6 Steady-State Flight 185

    3.7 Numerical Linearization 199

    3.8 Aircraft Dynamic Behavior 205

    3.9 Feedback Control 213

    3.10 Summary 241

    References 241

    Problems 243

    4 Aircraft Dynamics and Classical Control Design 250

    4.1 Introduction 250

    4.2 Aircraft Rigid-Body Modes 257

    4.3 The Handling-Qualities Requirements 274

    4.4 Stability Augmentation 287

    4.5 Control Augmentation Systems 303

    4.6 Autopilots 322

    4.7 Nonlinear Simulation 344

    4.8 Summary 371

    References 372

    Problems 374

    5 Modern Design Techniques 377

    5.1 Introduction 377

    5.2 Assignment of Closed-Loop Dynamics 381

    5.3 Linear Quadratic Regulator With Output Feedback 397

    5.4 Tracking A Command 413

    5.5 Modifying The Performance Index 428

    5.6 Model-Following Design 455

    5.7 Linear Quadratic Design with Full State Feedback 470

    5.8 Dynamic Inversion Design 477

    5.9 Summary 492

    References 492

    Problems 495

    6 Robustness and Multivariable Frequency-Domain Techniques 500

    6.1 Introduction 500

    6.2 Multivariable Frequency-Domain Analysis 502

    6.3 Robust Output-Feedback Design 525

    6.4 Observers and The Kalman Filter 529

    6.5 Linear Quadratic Gaussian/Loop Transfer Recovery 554

    6.6 Summary 577

    References 578

    Problems 580

    7 Digital Control 584

    7.1 Introduction 584

    7.2 Simulation of Digital Controllers 585

    7.3 Discretization of Continuous Controllers 588

    7.4 Modified Continuous Design 598

    7.5 Implementation Considerations 611

    7.6 Summary 619

    References 620

    Problems 620

    8 Modeling and Simulation of Miniature Aerial Vehicles 623

    8.1 Introduction 623

    8.2 Propeller/Rotor Forces and Moments 630

    8.3 Modeling Rotor Flapping 640

    8.4 Motor Modeling 645

    8.5 Small Aerobatic Airplane Model 648

    8.6 Quadrotor Model 654

    8.7 Small Helicopter Model 655

    8.8 Summary 660

    References 661

    Problems 661

    9 Adaptive Control with Application to Miniature Aerial Vehicles 664

    9.1 Introduction 664

    9.2 Model Reference Adaptive Control Based On Dynamic Inversion 665

    9.3 Neural Network Adaptive Control 668

    9.4 Limited Authority Adaptive Control 674

    9.5 Neural Network Adaptive Control Example 680

    9.6 Summary 709

    References 709

    Problems 711

    Appendix A F-16 Model 714

    Appendix B Software 723

    Index 733