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Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems 3rd edition [Kõva köide]

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(Georgia Tech Research Institute), (Georgia Institute of Technology),
  • Formaat: Hardback, 768 pages, kõrgus x laius x paksus: 236x163x43 mm, kaal: 1021 g
  • Ilmumisaeg: 26-Feb-2016
  • Kirjastus: Wiley-Blackwell
  • ISBN-10: 1118870980
  • ISBN-13: 9781118870983
Teised raamatud teemal:
Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems 3rd editionSuurem pilt
  • Formaat: Hardback, 768 pages, kõrgus x laius x paksus: 236x163x43 mm, kaal: 1021 g
  • Ilmumisaeg: 26-Feb-2016
  • Kirjastus: Wiley-Blackwell
  • ISBN-10: 1118870980
  • ISBN-13: 9781118870983
Teised raamatud teemal:
Püsilink: https://www.kriso.ee/db/9781118870983.html
Märksõnad:
Get a complete understanding of aircraft control and simulation

Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems, Third Edition is a comprehensive guide to aircraft control and simulation. This updated text covers flight control systems, flight dynamics, aircraft modeling, and flight simulation from both classical design and modern perspectives, as well as two new chapters on the modeling, simulation, and adaptive control of unmanned aerial vehicles. With detailed examples, including relevant MATLAB calculations and FORTRAN codes, this approachable yet detailed reference also provides access to supplementary materials, including chapter problems and an instructor's solution manual.

Aircraft control, as a subject area, combines an understanding of aerodynamics with knowledge of the physical systems of an aircraft. The ability to analyze the performance of an aircraft both in the real world and in computer-simulated flight is essential to maintaining proper control and function of the aircraft. Keeping up with the skills necessary to perform this analysis is critical for you to thrive in the aircraft control field.

  • Explore a steadily progressing list of topics, including equations of motion and aerodynamics, classical controls, and more advanced control methods
  • Consider detailed control design examples using computer numerical tools and simulation examples
  • Understand control design methods as they are applied to aircraft nonlinear math models
  • Access updated content about unmanned aircraft (UAVs)

Aircraft Control and Simulation: Dynamics, Controls Design, and Autonomous Systems, Third Edition is an essential reference for engineers and designers involved in the development of aircraft and aerospace systems and computer-based flight simulations, as well as upper-level undergraduate and graduate students studying mechanical and aerospace engineering.

Arvustused

The book retains its original chapter subject skeleton with the titles slightly changed and as mentioned has two new chapters added, in total it is some 150 pages longer than the original. This is not however a simple graft of new material onto the original book. Many of the chapters have been rewritten so that even where much the same material is covered, it is more detailed and augmented, whilst at the same time maintaining a consistent uniform style across the whole book....In conclusion this new edition is a significant update of a popular text...(The Aeronautical Journal- January 2017)

Preface xi
1 The Kinematics and Dynamics of Aircraft Motion 1(62)
1.1 Introduction
1(2)
1.2 Vector Operations
3(4)
1.3 Matrix Operations on Vector Coordinates
7(9)
1.4 Rotational Kinematics
16(4)
1.5 Translational Kinematics
20(3)
1.6 Geodesy, Coordinate Systems, Gravity
23(11)
1.7 Rigid-Body Dynamics
34(10)
1.8 Advanced Topics
44(14)
References
58(1)
Problems
59(4)
2 Modeling the Aircraft 63(79)
2.1 Introduction
63(1)
2.2 Basic Aerodynamics
64(11)
2.3 Aircraft Forces And Moments
75(26)
2.4 Static Analysis
101(7)
2.5 The Nonlinear Aircraft Model
108(8)
2.6 Linear Models And The Stability Derivatives
116(21)
2.7 Summary
137(1)
References
138(1)
Problems
139(3)
3 Modeling, Design, and Simulation Tools 142(108)
3.1 Introduction
142(2)
3.2 State-Space Models
144(11)
3.3 Transfer Function Models
155(15)
3.4 Numerical Solution Of The State Equations
170(9)
3.5 Aircraft Models For Simulation
179(6)
3.6 Steady-State Flight
185(14)
3.7 Numerical Linearization
199(6)
3.8 Aircraft Dynamic Behavior
205(8)
3.9 Feedback Control
213(28)
3.10 Summary
241(1)
References
241(2)
Problems
243(7)
4 Aircraft Dynamics and Classical Control Design 250(127)
4.1 Introduction
250(7)
4.2 Aircraft Rigid-Body Modes
257(17)
4.3 The Handling-Qualities Requirements
274(13)
4.4 Stability Augmentation
287(16)
4.5 Control Augmentation Systems
303(19)
4.6 Autopilots
322(22)
4.7 Nonlinear Simulation
344(27)
4.8 Summary
371(1)
References
372(2)
Problems
374(3)
5 Modern Design Techniques 377(123)
5.1 Introduction
377(4)
5.2 Assignment Of Closed-Loop Dynamics
381(16)
5.3 Linear Quadratic Regulator With Output Feedback
397(16)
5.4 Tracking A Command
413(15)
5.5 Modifying The Performance Index
428(27)
5.6 Model-Following Design
455(15)
5.7 Linear Quadratic Design With Full State Feedback
470(7)
5.8 Dynamic Inversion Design
477(15)
5.9 Summary
492(1)
References
492(3)
Problems
495(5)
6 Robustness and Multivariable Frequency-Domain Techniques 500(84)
6.1 Introduction
500(2)
6.2 Multivariable Frequency-Domain Analysis
502(23)
6.3 Robust Output-Feedback Design
525(4)
6.4 Observers And The Kalman Filter
529(25)
6.5 Linear Quadratic Gaussian/Loop Transfer Recovery
554(23)
6.6 Summary
577(1)
References
578(2)
Problems
580(4)
7 Digital Control 584(39)
7.1 Introduction
584(1)
7.2 Simulation Of Digital Controllers
585(3)
7.3 Discretization Of Continuous Controllers
588(10)
7.4 Modified Continuous Design
598(13)
7.5 Implementation Considerations
611(8)
7.6 Summary
619(1)
References
620(1)
Problems
620(3)
8 Modeling and Simulation of Miniature Aerial Vehicles 623(41)
8.1 Introduction
623(7)
8.2 Propeller/Rotor Forces And Moments
630(10)
8.3 Modeling Rotor Flapping
640(5)
8.4 Motor Modeling
645(3)
8.5 Small Aerobatic Airplane Model
648(6)
8.6 Quadrotor Model
654(1)
8.7 Small Helicopter Model
655(5)
8.8 Summary
660(1)
References
661(1)
Problems
661(3)
9 Adaptive Control With Application to Miniature Aerial Vehicles 664(50)
9.1 Introduction
664(1)
9.2 Model Reference Adaptive Control Based On Dynamic Inversion
665(3)
9.3 Neural Network Adaptive Control
668(6)
9.4 Limited Authority Adaptive Control
674(6)
9.5 Neural Network Adaptive Control Example
680(29)
9.6 Summary
709(1)
References
709(2)
Problems
711(3)
Appendix A F-16 Model 714(9)
Appendix B Software 723(10)
Index 733
BRIAN L. STEVENS is a retired Senior Research Engineer from the Georgia Institute of Technology Research Institute, where he continues to teach classes in Guidance, Navigation, and Control.

FRANK L. LEWIS is a Distinguished Scholar Professor, Distinguished Teaching Professor, and Moncrief-O'Donnell Chair at the University of Texas at Arlington Research Institute.

ERIC N. JOHNSON is the Lockheed Martin Associate Professor of Avionics Integration, Daniel Guggenheim School of Aerospace Engineering at Georgia Institute of Technology.