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Flight dynamics principles [[electronic resource] ] : [a linear systems approach to aircraft stability and control] / / M.V. Cook
| Flight dynamics principles [[electronic resource] ] : [a linear systems approach to aircraft stability and control] / / M.V. Cook |
| Autore | Cook M. V |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 |
| Descrizione fisica | 1 online resource (491 p.) |
| Disciplina |
629.1
629.1323 |
| Collana | Elsevier aerospace engineering series |
| Soggetto topico | Aerodynamics |
| Soggetto genere / forma | Electronic books. |
| ISBN |
1-281-02927-0
9786611029272 0-08-055036-3 |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front cover; Flight Dynamics Principles; Copyright page; Contents; Preface to the first edition; Preface to the second edition; Acknowledgements; Nomenclature; Chapter 1. Introduction; 1.1 Overview; 1.2 Flying and handling qualities; 1.3 General considerations; 1.4 Aircraft equations of motion; 1.5 Aerodynamics; 1.6 Computers; 1.7 Summary; References; Chapter 2. Systems of axes and notation; 2.1 Earth axes; 2.2 Aircraft body fixed axes; 2.3 Euler angles and aircraft attitude; 2.4 Axes transformations; 2.5 Aircraft reference geometry; 2.6 Controls notation; 2.7 Aerodynamic reference centres
ReferencesProblems; Chapter 3. Static equilibrium and trim; 3.1 Trim equilibrium; 3.2 The pitching moment equation; 3.3 Longitudinal static stability; 3.4 Lateral static stability; 3.5 Directional static stability; 3.6 Calculation of aircraft trim condition; References; Problems; Chapter 4. The equations of motion; 4.1 The equations of motion of a rigid symmetric aircraft; 4.2 The linearised equations of motion; 4.3 The decoupled equations of motion; 4.4 Alternative forms of the equations of motion; References; Problems; Chapter 5. The solution of the equations of motion 5.1 Methods of solution5.2 Cramer's rule; 5.3 Aircraft response transfer functions; 5.4 Response to controls; 5.5 Acceleration response transfer functions; 5.6 The state space method; 5.7 State space model augmentation; References; Problems; Chapter 6. Longitudinal dynamics; 6.1 Response to controls; 6.2 The dynamic stability modes; 6.3 Reduced order models; 6.4 Frequency response; 6.5 Flying and handling qualities; 6.6 Mode excitation; References; Problems; Chapter 7. Lateral-directional dynamics; 7.1 Response to controls; 7.2 The dynamic stability modes; 7.3 Reduced order models 7.4 Frequency response7.5 Flying and handling qualities; 7.6 Mode excitation; References; Problems; Chapter 8. Manoeuvrability; 8.1 Introduction; 8.2 The steady pull-up manoeuvre; 8.3 The pitching moment equation; 8.4 Longitudinal manoeuvre stability; 8.5 Aircraft dynamics and manoeuvrability; References; Chapter 9. Stability; 9.1 Introduction; 9.2 The characteristic equation; 9.3 The Routh-Hurwitz stability criterion; 9.4 The stability quartic; 9.5 Graphical interpretation of stability; References; Problems; Chapter 10. Flying and handling qualities; 10.1 Introduction 10.2 Short term dynamic models10.3 Flying qualities requirements; 10.4 Aircraft role; 10.5 Pilot opinion rating; 10.6 Longitudinal flying qualities requirements; 10.7 Control anticipation parameter; 10.8 Lateral-directional flying qualities requirements; 10.9 Flying qualities requirements on the s-plane; References; Problems; Chapter 11. Stability augmentation; 11.1 Introduction; 11.2 Augmentation system design; 11.3 Closed loop system analysis; 11.4 The root locus plot; 11.5 Longitudinal stability augmentation; 11.6 Lateral-directional stability augmentation; 11.7 The pole placement method References |
| Record Nr. | UNINA-9910457685103321 |
Cook M. V
|
||
| Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Flight dynamics principles [[electronic resource] ] : [a linear systems approach to aircraft stability and control] / / M.V. Cook
| Flight dynamics principles [[electronic resource] ] : [a linear systems approach to aircraft stability and control] / / M.V. Cook |
| Autore | Cook M. V |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 |
| Descrizione fisica | 1 online resource (491 p.) |
| Disciplina |
629.1
629.1323 |
| Collana | Elsevier aerospace engineering series |
| Soggetto topico |
Aerodynamics
Flight Stability of airplanes |
| ISBN |
1-281-02927-0
9786611029272 0-08-055036-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front cover; Flight Dynamics Principles; Copyright page; Contents; Preface to the first edition; Preface to the second edition; Acknowledgements; Nomenclature; Chapter 1. Introduction; 1.1 Overview; 1.2 Flying and handling qualities; 1.3 General considerations; 1.4 Aircraft equations of motion; 1.5 Aerodynamics; 1.6 Computers; 1.7 Summary; References; Chapter 2. Systems of axes and notation; 2.1 Earth axes; 2.2 Aircraft body fixed axes; 2.3 Euler angles and aircraft attitude; 2.4 Axes transformations; 2.5 Aircraft reference geometry; 2.6 Controls notation; 2.7 Aerodynamic reference centres
ReferencesProblems; Chapter 3. Static equilibrium and trim; 3.1 Trim equilibrium; 3.2 The pitching moment equation; 3.3 Longitudinal static stability; 3.4 Lateral static stability; 3.5 Directional static stability; 3.6 Calculation of aircraft trim condition; References; Problems; Chapter 4. The equations of motion; 4.1 The equations of motion of a rigid symmetric aircraft; 4.2 The linearised equations of motion; 4.3 The decoupled equations of motion; 4.4 Alternative forms of the equations of motion; References; Problems; Chapter 5. The solution of the equations of motion 5.1 Methods of solution5.2 Cramer's rule; 5.3 Aircraft response transfer functions; 5.4 Response to controls; 5.5 Acceleration response transfer functions; 5.6 The state space method; 5.7 State space model augmentation; References; Problems; Chapter 6. Longitudinal dynamics; 6.1 Response to controls; 6.2 The dynamic stability modes; 6.3 Reduced order models; 6.4 Frequency response; 6.5 Flying and handling qualities; 6.6 Mode excitation; References; Problems; Chapter 7. Lateral-directional dynamics; 7.1 Response to controls; 7.2 The dynamic stability modes; 7.3 Reduced order models 7.4 Frequency response7.5 Flying and handling qualities; 7.6 Mode excitation; References; Problems; Chapter 8. Manoeuvrability; 8.1 Introduction; 8.2 The steady pull-up manoeuvre; 8.3 The pitching moment equation; 8.4 Longitudinal manoeuvre stability; 8.5 Aircraft dynamics and manoeuvrability; References; Chapter 9. Stability; 9.1 Introduction; 9.2 The characteristic equation; 9.3 The Routh-Hurwitz stability criterion; 9.4 The stability quartic; 9.5 Graphical interpretation of stability; References; Problems; Chapter 10. Flying and handling qualities; 10.1 Introduction 10.2 Short term dynamic models10.3 Flying qualities requirements; 10.4 Aircraft role; 10.5 Pilot opinion rating; 10.6 Longitudinal flying qualities requirements; 10.7 Control anticipation parameter; 10.8 Lateral-directional flying qualities requirements; 10.9 Flying qualities requirements on the s-plane; References; Problems; Chapter 11. Stability augmentation; 11.1 Introduction; 11.2 Augmentation system design; 11.3 Closed loop system analysis; 11.4 The root locus plot; 11.5 Longitudinal stability augmentation; 11.6 Lateral-directional stability augmentation; 11.7 The pole placement method References |
| Record Nr. | UNINA-9910784357203321 |
|
Cook M. V
|
||
| Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||
Flight dynamics principles : [a linear systems approach to aircraft stability and control] / / M.V. Cook
| Flight dynamics principles : [a linear systems approach to aircraft stability and control] / / M.V. Cook |
| Autore | Cook M. V |
| Edizione | [2nd ed.] |
| Pubbl/distr/stampa | Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 |
| Descrizione fisica | 1 online resource (491 p.) |
| Disciplina |
629.1
629.1323 |
| Collana | Elsevier aerospace engineering series |
| Soggetto topico |
Aerodynamics
Flight Stability of airplanes |
| ISBN |
1-281-02927-0
9786611029272 0-08-055036-3 |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Nota di contenuto |
Front cover; Flight Dynamics Principles; Copyright page; Contents; Preface to the first edition; Preface to the second edition; Acknowledgements; Nomenclature; Chapter 1. Introduction; 1.1 Overview; 1.2 Flying and handling qualities; 1.3 General considerations; 1.4 Aircraft equations of motion; 1.5 Aerodynamics; 1.6 Computers; 1.7 Summary; References; Chapter 2. Systems of axes and notation; 2.1 Earth axes; 2.2 Aircraft body fixed axes; 2.3 Euler angles and aircraft attitude; 2.4 Axes transformations; 2.5 Aircraft reference geometry; 2.6 Controls notation; 2.7 Aerodynamic reference centres
ReferencesProblems; Chapter 3. Static equilibrium and trim; 3.1 Trim equilibrium; 3.2 The pitching moment equation; 3.3 Longitudinal static stability; 3.4 Lateral static stability; 3.5 Directional static stability; 3.6 Calculation of aircraft trim condition; References; Problems; Chapter 4. The equations of motion; 4.1 The equations of motion of a rigid symmetric aircraft; 4.2 The linearised equations of motion; 4.3 The decoupled equations of motion; 4.4 Alternative forms of the equations of motion; References; Problems; Chapter 5. The solution of the equations of motion 5.1 Methods of solution5.2 Cramer's rule; 5.3 Aircraft response transfer functions; 5.4 Response to controls; 5.5 Acceleration response transfer functions; 5.6 The state space method; 5.7 State space model augmentation; References; Problems; Chapter 6. Longitudinal dynamics; 6.1 Response to controls; 6.2 The dynamic stability modes; 6.3 Reduced order models; 6.4 Frequency response; 6.5 Flying and handling qualities; 6.6 Mode excitation; References; Problems; Chapter 7. Lateral-directional dynamics; 7.1 Response to controls; 7.2 The dynamic stability modes; 7.3 Reduced order models 7.4 Frequency response7.5 Flying and handling qualities; 7.6 Mode excitation; References; Problems; Chapter 8. Manoeuvrability; 8.1 Introduction; 8.2 The steady pull-up manoeuvre; 8.3 The pitching moment equation; 8.4 Longitudinal manoeuvre stability; 8.5 Aircraft dynamics and manoeuvrability; References; Chapter 9. Stability; 9.1 Introduction; 9.2 The characteristic equation; 9.3 The Routh-Hurwitz stability criterion; 9.4 The stability quartic; 9.5 Graphical interpretation of stability; References; Problems; Chapter 10. Flying and handling qualities; 10.1 Introduction 10.2 Short term dynamic models10.3 Flying qualities requirements; 10.4 Aircraft role; 10.5 Pilot opinion rating; 10.6 Longitudinal flying qualities requirements; 10.7 Control anticipation parameter; 10.8 Lateral-directional flying qualities requirements; 10.9 Flying qualities requirements on the s-plane; References; Problems; Chapter 11. Stability augmentation; 11.1 Introduction; 11.2 Augmentation system design; 11.3 Closed loop system analysis; 11.4 The root locus plot; 11.5 Longitudinal stability augmentation; 11.6 Lateral-directional stability augmentation; 11.7 The pole placement method References |
| Record Nr. | UNINA-9910825103603321 |
|
Cook M. V
|
||
| Oxford [UK] ; ; Burlington, MA, : Butterworth-Heinemann/Elsevier, 2007 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
| ||