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Aircraft dynamic stability and response / / A. W. Babister
| Aircraft dynamic stability and response / / A. W. Babister |
| Autore | Babister A. W. |
| Edizione | [First edition.] |
| Pubbl/distr/stampa | Oxford, England : , : Pergamon Press, , 1986 |
| Descrizione fisica | 1 online resource (247 p.) |
| Disciplina | 629.13236 |
| Collana | Pergamon International Library of Science, Technology, Engineering and Social Studies |
| Soggetto topico |
Stability of airplanes
Airplanes - Handling characteristics |
| ISBN | 1-4831-4035-0 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Aircraft Dynamic Stability and Response; Copyright Page; Table of Contents; Preface; List Of Symbols; NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICA; UNITS; Part I: FLIGHT DYNAMICS; Chapter 1.INTRODUCTION; THE GENERAL MEANING OF STABILITY; LONGITUDINAL STATIC STABILITY; STATIC MARGIN; STABILITY AND TRIM; MANOEUVRABILITY AND MANOEUVRE MARGIN; REFERENCES; PROBLEMS; Chapter 2. THE EQUATIONS OF MOTION; INTRODUCTION; THE GENERAL DYNAMICAL EQUATIONS FOR A RIGID AIRCRAFT REFERRED TO MOVING AXES
DEFINITION OF THE ANGLE OF PITCH θ, THE ANGLE OF BANK Φ AND ANGLE OF YAW ψRELATIONS FOR RATES OF ROLL, PITCH AND YAW; DETERMINATION OF THE GRAVITATIONAL FORCES; ANGLES OF YAW AND SIDESLIP; DETERMINATION OF THE AERODYNAMIC FORCES; SEPARABILITY OF LONGITUDINAL AND LATERAL MOTION; AXIS SYSTEMS USED IN STABILITY ANALYSIS; NON-DIMENSIONAL AERODYNAMIC DERIVATIVES (LONGITUDINAL); NON-DIMENSIONAL AERODYNAMIC DERIVATIVES (LATERAL); NON-DIMENSIONAL DISTURBANCES; NON-DIMENSIONAL MASS AND INERTIA; NON-DIMENSIONAL FORM OF THE EQUATIONS OF MOTION; THE MOTION OF THE CENTRE OF GRAVITY OF THE AIRCRAFT REFERENCESPROBLEMS; Chapter 3. AERODYNAMIC DERIVATIVES (LONGITUDINAL); INTRODUCTION; FORCE VELOCITY DERIVATIVES Xu, Xw, Zu, Zw; INCIDENCE CHANGE ASSOCIATED WITH CHANGE IN VELOCITY COMPONENTS; PITCHING MOMENT DERIVATIVES Mu, Mw; DERIVATIVES DUE TO RATE OF PITCH Xq, Zq, Mq; DERIVATIVES DUE TO RATE OF CHANGE OF DOWNWARD VELOCITY X'w, Z'w, M'w; CONTROL DERIVATIVES; NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICA; AMERICAN NON-DIMENSIONAL FORCE-VELOCITY DERIVATIVES cxu, cxα, czu, czα,; AMERICAN NON-DIMENSIONAL PITCHING MOMENT DERIVATIVES Cmu, Cma AMERICAN NON-DIMENSIONAL DERIVATIVES DUE TO RATE OF PITCH cxq, czq, cmqAMERICAN NON-DIMENSIONAL DERIVATIVES DUE TO RATE OF CHANGE OF DOWNWARD VELOCITY CxDα, CzDα, CmDα; AMERICAN NON-DIMENSIONAL CONTROL DERIVATIVES Cxδe, CZδe, Cmδe DUE TO ELEVATOR; REFERENCES; PROBLEMS; Chapter 4. AERODYNAMIC DERIVATIVES (LATERAL); INTRODUCTION; ESTIMATION OF LATERAL STABILITY DERIVATIVES; DERIVATIVES DUE TO SIDESLIP; DERIVATIVES DUE TO RATE OF ROLL; DERIVATIVES DUE TO RATE OF YAW; CONTROL DERIVATIVES; DERIVATIVES DUE TO AILERONS; DERIVATIVES DUE TO RUDDER NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICANON-DIMENSIONAL FORMS OF THE CONTROL DERIVATIVES USED IN AMERICA; REFERENCES; PROBLEMS; Part II: LONGITUDINAL DYNAMIC STABILITY AND RESPONSE; Chapter 5. BASIC LONGITUDINAL MOTIONS; INTRODUCTION; THE SHORT PERIOD OSCILLATION; THE PHUGOID (LONG PERIOD) OSCILLATION; PROBLEMS; Chapter 6. LONGITUDINAL DYNAMIC STABILITY; INTRODUCTION; STICK FIXED DYNAMIC STABILITY; THE GENERAL SOLUTION OF THE EQUATIONS OF MOTION; TYPES OF MOTION CORRESPONDING TO THE ROOTS OF THE CHARACTERISTIC EQUATION ANALYSIS OF THE ROOTS OF THE CHARACTERISTIC EQUATION |
| Record Nr. | UNINA-9910789585803321 |
Babister A. W.
|
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| Oxford, England : , : Pergamon Press, , 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Aircraft dynamic stability and response / / A. W. Babister
| Aircraft dynamic stability and response / / A. W. Babister |
| Autore | Babister A. W. |
| Edizione | [First edition.] |
| Pubbl/distr/stampa | Oxford, England : , : Pergamon Press, , 1986 |
| Descrizione fisica | 1 online resource (247 p.) |
| Disciplina | 629.13236 |
| Collana | Pergamon International Library of Science, Technology, Engineering and Social Studies |
| Soggetto topico |
Stability of airplanes
Airplanes - Handling characteristics |
| ISBN | 1-4831-4035-0 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front Cover; Aircraft Dynamic Stability and Response; Copyright Page; Table of Contents; Preface; List Of Symbols; NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICA; UNITS; Part I: FLIGHT DYNAMICS; Chapter 1.INTRODUCTION; THE GENERAL MEANING OF STABILITY; LONGITUDINAL STATIC STABILITY; STATIC MARGIN; STABILITY AND TRIM; MANOEUVRABILITY AND MANOEUVRE MARGIN; REFERENCES; PROBLEMS; Chapter 2. THE EQUATIONS OF MOTION; INTRODUCTION; THE GENERAL DYNAMICAL EQUATIONS FOR A RIGID AIRCRAFT REFERRED TO MOVING AXES
DEFINITION OF THE ANGLE OF PITCH θ, THE ANGLE OF BANK Φ AND ANGLE OF YAW ψRELATIONS FOR RATES OF ROLL, PITCH AND YAW; DETERMINATION OF THE GRAVITATIONAL FORCES; ANGLES OF YAW AND SIDESLIP; DETERMINATION OF THE AERODYNAMIC FORCES; SEPARABILITY OF LONGITUDINAL AND LATERAL MOTION; AXIS SYSTEMS USED IN STABILITY ANALYSIS; NON-DIMENSIONAL AERODYNAMIC DERIVATIVES (LONGITUDINAL); NON-DIMENSIONAL AERODYNAMIC DERIVATIVES (LATERAL); NON-DIMENSIONAL DISTURBANCES; NON-DIMENSIONAL MASS AND INERTIA; NON-DIMENSIONAL FORM OF THE EQUATIONS OF MOTION; THE MOTION OF THE CENTRE OF GRAVITY OF THE AIRCRAFT REFERENCESPROBLEMS; Chapter 3. AERODYNAMIC DERIVATIVES (LONGITUDINAL); INTRODUCTION; FORCE VELOCITY DERIVATIVES Xu, Xw, Zu, Zw; INCIDENCE CHANGE ASSOCIATED WITH CHANGE IN VELOCITY COMPONENTS; PITCHING MOMENT DERIVATIVES Mu, Mw; DERIVATIVES DUE TO RATE OF PITCH Xq, Zq, Mq; DERIVATIVES DUE TO RATE OF CHANGE OF DOWNWARD VELOCITY X'w, Z'w, M'w; CONTROL DERIVATIVES; NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICA; AMERICAN NON-DIMENSIONAL FORCE-VELOCITY DERIVATIVES cxu, cxα, czu, czα,; AMERICAN NON-DIMENSIONAL PITCHING MOMENT DERIVATIVES Cmu, Cma AMERICAN NON-DIMENSIONAL DERIVATIVES DUE TO RATE OF PITCH cxq, czq, cmqAMERICAN NON-DIMENSIONAL DERIVATIVES DUE TO RATE OF CHANGE OF DOWNWARD VELOCITY CxDα, CzDα, CmDα; AMERICAN NON-DIMENSIONAL CONTROL DERIVATIVES Cxδe, CZδe, Cmδe DUE TO ELEVATOR; REFERENCES; PROBLEMS; Chapter 4. AERODYNAMIC DERIVATIVES (LATERAL); INTRODUCTION; ESTIMATION OF LATERAL STABILITY DERIVATIVES; DERIVATIVES DUE TO SIDESLIP; DERIVATIVES DUE TO RATE OF ROLL; DERIVATIVES DUE TO RATE OF YAW; CONTROL DERIVATIVES; DERIVATIVES DUE TO AILERONS; DERIVATIVES DUE TO RUDDER NON-DIMENSIONAL FORMS OF THE AERODYNAMIC DERIVATIVES USED IN AMERICANON-DIMENSIONAL FORMS OF THE CONTROL DERIVATIVES USED IN AMERICA; REFERENCES; PROBLEMS; Part II: LONGITUDINAL DYNAMIC STABILITY AND RESPONSE; Chapter 5. BASIC LONGITUDINAL MOTIONS; INTRODUCTION; THE SHORT PERIOD OSCILLATION; THE PHUGOID (LONG PERIOD) OSCILLATION; PROBLEMS; Chapter 6. LONGITUDINAL DYNAMIC STABILITY; INTRODUCTION; STICK FIXED DYNAMIC STABILITY; THE GENERAL SOLUTION OF THE EQUATIONS OF MOTION; TYPES OF MOTION CORRESPONDING TO THE ROOTS OF THE CHARACTERISTIC EQUATION ANALYSIS OF THE ROOTS OF THE CHARACTERISTIC EQUATION |
| Record Nr. | UNINA-9910819946403321 |
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Babister A. W.
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| Oxford, England : , : Pergamon Press, , 1986 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Airplane performance stability and control / Courtland D. Perkins, Robert E. Hage
| Airplane performance stability and control / Courtland D. Perkins, Robert E. Hage |
| Autore | Perkins, Courtland D. |
| Pubbl/distr/stampa | New York [etc.] : J. Wiley, 1949 |
| Descrizione fisica | VII, 493 p. : ill. ; 23 cm |
| Disciplina | 629.13236 |
| Altri autori (Persone) | Hage, Robert E. |
| Soggetto non controllato | AeroplaniVolo |
| ISBN | 0-471-68046-X |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Titolo uniforme | |
| Record Nr. | UNIPARTHENOPE-000022186 |
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Perkins, Courtland D.
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| New York [etc.] : J. Wiley, 1949 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Parthenope | ||
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Dynamics of atmospheric flight / Bernard Etkin
| Dynamics of atmospheric flight / Bernard Etkin |
| Autore | Etkin, Bernard |
| Pubbl/distr/stampa | New York [etc.], : J. Wiley, c1972 |
| Descrizione fisica | XIII, 579 p. : ill. ; 24 cm. |
| Disciplina |
629.132
629.13236 |
| Soggetto topico |
Aerodinamica
Aeroplani - Stabilità Aeroplani - Volo |
| ISBN | 0471246204 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISANNIO-SBL0192415 |
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Etkin, Bernard
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| New York [etc.], : J. Wiley, c1972 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. del Sannio | ||
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Dynamics of flight : stability and control / Bernard Etkin, Lloyd Duff Reid
| Dynamics of flight : stability and control / Bernard Etkin, Lloyd Duff Reid |
| Autore | Etkin, Bernard |
| Edizione | [3. ed] |
| Pubbl/distr/stampa | New York [etc.], : Wiley, c1996 |
| Descrizione fisica | XI, 382 p. : ill. ; 26 cm. |
| Disciplina |
629.132
629.13236 |
| Altri autori (Persone) | Reid, Lloyd Duff |
| Soggetto topico |
Aerodinamica
Aeroplani - Stabilità Aeroplani - Volo |
| ISBN | 0471034185 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNISANNIO-MIL0291869 |
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Etkin, Bernard
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| New York [etc.], : Wiley, c1996 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. del Sannio | ||
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Fundamentals and applications of modern flow control [[electronic resource] /] / edited by Ronald D. Joslin, Daniel N. Miller
| Fundamentals and applications of modern flow control [[electronic resource] /] / edited by Ronald D. Joslin, Daniel N. Miller |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 2009 |
| Descrizione fisica | 1 online resource (550 p.) |
| Disciplina | 629.13236 |
| Altri autori (Persone) |
JoslinRonald D
MillerDaniel N |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Fluid dynamics
Hydraulic control |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-56347-989-3
1-56347-988-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover ""; ""Title ""; ""Copyright ""; ""Foreword ""; ""Table of Contents ""; ""Nomenclature ""; ""Acronyms and Abbreviations ""; ""Preface ""; ""Acknowledgements ""; ""Brief History of Flow Control""; ""Physical Concepts Underlying the Development and Application of Active Flow Control""; ""Flow Control Terminology""; ""Role of Instability Theory in Flow Control""; ""Dynamic and Closed-Loop Control""; ""Actuators and Sensors""; ""Modeling and Simulation ""; ""Fixed Wing Airfoil Applications ""; ""Turbomachinery Applications""; ""Combustion Control""; ""Aeroacoustics of Flow Control""
""Air-Breathing Propulsion Flowpath Applications""""Flow Control for Rotorcraft Applications""; ""References""; ""Index""; ""Supporting Materials"" |
| Record Nr. | UNINA-9910457651903321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 2009 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Fundamentals and applications of modern flow control [[electronic resource] /] / edited by Ronald D. Joslin, Daniel N. Miller
| Fundamentals and applications of modern flow control [[electronic resource] /] / edited by Ronald D. Joslin, Daniel N. Miller |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 2009 |
| Descrizione fisica | 1 online resource (550 p.) |
| Disciplina | 629.13236 |
| Altri autori (Persone) |
JoslinRonald D
MillerDaniel N |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Fluid dynamics
Hydraulic control |
| ISBN |
1-56347-989-3
1-56347-988-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover ""; ""Title ""; ""Copyright ""; ""Foreword ""; ""Table of Contents ""; ""Nomenclature ""; ""Acronyms and Abbreviations ""; ""Preface ""; ""Acknowledgements ""; ""Brief History of Flow Control""; ""Physical Concepts Underlying the Development and Application of Active Flow Control""; ""Flow Control Terminology""; ""Role of Instability Theory in Flow Control""; ""Dynamic and Closed-Loop Control""; ""Actuators and Sensors""; ""Modeling and Simulation ""; ""Fixed Wing Airfoil Applications ""; ""Turbomachinery Applications""; ""Combustion Control""; ""Aeroacoustics of Flow Control""
""Air-Breathing Propulsion Flowpath Applications""""Flow Control for Rotorcraft Applications""; ""References""; ""Index""; ""Supporting Materials"" |
| Record Nr. | UNINA-9910781431103321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 2009 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Fundamentals and applications of modern flow control [[electronic resource] /] / edited by Ronald D. Joslin, Daniel N. Miller
| Fundamentals and applications of modern flow control [[electronic resource] /] / edited by Ronald D. Joslin, Daniel N. Miller |
| Pubbl/distr/stampa | Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 2009 |
| Descrizione fisica | 1 online resource (550 p.) |
| Disciplina | 629.13236 |
| Altri autori (Persone) |
JoslinRonald D
MillerDaniel N |
| Collana | Progress in astronautics and aeronautics |
| Soggetto topico |
Fluid dynamics
Hydraulic control |
| ISBN |
1-56347-989-3
1-56347-988-5 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
""Cover ""; ""Title ""; ""Copyright ""; ""Foreword ""; ""Table of Contents ""; ""Nomenclature ""; ""Acronyms and Abbreviations ""; ""Preface ""; ""Acknowledgements ""; ""Brief History of Flow Control""; ""Physical Concepts Underlying the Development and Application of Active Flow Control""; ""Flow Control Terminology""; ""Role of Instability Theory in Flow Control""; ""Dynamic and Closed-Loop Control""; ""Actuators and Sensors""; ""Modeling and Simulation ""; ""Fixed Wing Airfoil Applications ""; ""Turbomachinery Applications""; ""Combustion Control""; ""Aeroacoustics of Flow Control""
""Air-Breathing Propulsion Flowpath Applications""""Flow Control for Rotorcraft Applications""; ""References""; ""Index""; ""Supporting Materials"" |
| Record Nr. | UNINA-9910809685603321 |
| Reston, Va., : American Institute of Aeronautics and Astronautics, Inc., 2009 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Recent developments in high-speed transport : selected contributions from international conference on high-speed transport development 2022 / / edited by Dmitry Yu. Strelets and Oleg N. Korsun
| Recent developments in high-speed transport : selected contributions from international conference on high-speed transport development 2022 / / edited by Dmitry Yu. Strelets and Oleg N. Korsun |
| Edizione | [1st ed. 2023.] |
| Pubbl/distr/stampa | Singapore : , : Springer Nature Singapore Pte Ltd., , [2023] |
| Descrizione fisica | 1 online resource (IX, 227 p. 146 illus., 118 illus. in color.) |
| Disciplina | 629.13236 |
| Collana | Springer Aerospace Technology |
| Soggetto topico |
Air travel
High-speed aeronautics Supersonic transport planes |
| ISBN | 981-19-9010-7 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto | Preface -- Markets, requirements, concepts for the implementation of the new generation supersonic aircraft -- Functioning models, modeling, software and hardware platforms for solving problems of new generation supersonic aircraft -- Design solutions, design implementation, weight analysis -- Energy and power systems of new generation supersonic aircraft -- New materials, production technologies -- Artificial intelligence, predictive analytics -- Certification, operation, after-sales service. |
| Record Nr. | UNINA-9910686480703321 |
| Singapore : , : Springer Nature Singapore Pte Ltd., , [2023] | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Stability and control of aircraft systems [[electronic resource] ] : introduction to classical feedback control / / Roy Langton
| Stability and control of aircraft systems [[electronic resource] ] : introduction to classical feedback control / / Roy Langton |
| Autore | Langton Roy |
| Pubbl/distr/stampa | Chichester, England ; ; Hoboken, NJ, : Wiley, c2006 |
| Descrizione fisica | 1 online resource (256 p.) |
| Disciplina |
629.13236
629.83 |
| Collana | Aerospace series |
| Soggetto topico |
Stability of airplanes
Airplanes - Control |
| Soggetto genere / forma | Electronic books. |
| ISBN |
0-470-05848-X
1-280-72117-0 9786610721177 0-470-05849-8 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Stability and Control of AircraftSystems; Contents; Series Preface; Preface; 1 Developing the Foundation; 1.1 Engineering Units; 1.1.1 International System of Units (SI); 1.1.2 US/Imperial Units System; 1.1.3 Comparing the SI and US/Imperial Units Systems; 1.2 Block Diagrams; 1.2.1 Examples of Summation (or Comparison) Devices; 1.3 Differential Equations; 1.3.1 Using the 'D' Notation; 1.4 Spring-Mass System Example; 1.4.1 The Standard Form of Second-order System Transfer Function; 1.5 Primer on Complex Numbers; 1.5.1 The Complex Sinusoid; 1.6 Chapter Summary; 2 Closing the Loop
2.1 The Generic Closed Loop System2.1.1 The Simplest Form of Closed Loop System; 2.2 The Concept of Stability; 2.3 Response Testing of Control Systems; 2.4 The Integration Process; 2.5 Hydraulic Servo-actuator Example; 2.6 Calculating Frequency Response; 2.6.1 Frequency Response of a First-order Lag; 2.6.2 Frequency Response of a Second-order System; 2.7 Aircraft Flight Control System Example; 2.7.1 Control System Assumptions; 2.7.2 Open Loop Analysis; 2.7.3 Closed Loop Performance; 2.8 Alternative Graphical Methods for Response Analysis; 2.8.1 The Nyquist Diagram 2.8.2 Deriving Closed Loop Response from Nyquist Diagrams2.8.3 The Nichols Chart; 2.8.4 Graphical Methods - Summary Comments and Suggestions; 2.9 Chapter Summary; 3 Control System Compensation Techniques; 3.1 Control System Requirements; 3.2 Compensation Methods; 3.2.1 Proportional Plus Integral Control; 3.2.2 Proportional Plus Integral Plus Derivative Control; 3.2.3 Lead-Lag Compensation; 3.2.4 Lag-Lead Compensation; 3.2.5 Feedback Compensation; 3.3 Applications of Control Compensation; 3.3.1 Proportional Plus Integral Example; 3.3.2 Lead-Lag Compensation Example 3.3.3 Class 2 System Design Example3.4 Chapter Summary; 4 Introduction to Laplace Transforms; 4.1 An Overview of the Application of Laplace Transforms; 4.2 The Evolution of the Laplace Transform; 4.2.1 Proof of the General Case; 4.3 Applying Laplace Transforms to Linear Systems Analysis; 4.3.1 Partial Fractions; 4.4 Laplace Transforms - Summary of Key Points; 4.5 Root Locus; 4.5.1 Root Locus Construction Rules; 4.5.2 Connecting Root Locus to Conventional Linear Analysis; 4.6 Root Locus Example; 4.7 Chapter Summary; 5 Dealing with Nonlinearities; 5.1 Definition of Nonlinearity Types 5.2 Continuous Nonlinearities5.2.1 Engine Fuel Control System Example; 5.3 Discontinuous Nonlinearities; 5.3.1 Stability Analysis with Discontinuous Nonlinearities; 5.4 The Transport Delay; 5.5 Simulation; 5.6 Chapter Summary; 6 Electronic Controls; 6.1 Analog Electronic Controls; 6.1.1 The Operational Amplifier; 6.1.2 Building Analog Control Algorithms; 6.2 The Digital Computer as a Dynamic Control Element; 6.2.1 Signal Conversion; 6.2.2 Digital Controller Architectures; 6.3 The Stability Impact of Digital Controls; 6.4 Digital Control Design Example; 6.5 Creating Digital Control Algorithms 6.5.1 The Integrator |
| Record Nr. | UNINA-9910143736303321 |
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Langton Roy
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| Chichester, England ; ; Hoboken, NJ, : Wiley, c2006 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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