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Analysis of wind-tunnel data on directional stability and control / / by H.R. Pass
| Analysis of wind-tunnel data on directional stability and control / / by H.R. Pass |
| Autore | Pass H. R. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics ; , 1940 |
| Descrizione fisica | 1 online resource (33 pages, 19 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Stability of airplanes
Airplanes - Control Airplanes - Tail surfaces Wind tunnel testing |
| Formato | Materiale a stampa  |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717113903321 |
Pass H. R.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics ; , 1940 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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A dangerous seaplane landing condition / / by Thomas Carroll
| A dangerous seaplane landing condition / / by Thomas Carroll |
| Autore | Carroll Thomas |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1928 |
| Descrizione fisica | 1 online resource (3 pages) |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Seaplanes
Airplanes - Landing Airplanes - Control Aircraft accidents |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713664503321 |
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Carroll Thomas
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1928 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Flight investigation of control-stick vibration of the YG-1B autogiro / / by F.J. Bailey, Jr
| Flight investigation of control-stick vibration of the YG-1B autogiro / / by F.J. Bailey, Jr |
| Autore | Bailey F. J, Jr. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1940 |
| Descrizione fisica | 1 online resource (10 pages, 8 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Autogiros
Airplanes - Control Vibration |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717124403321 |
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Bailey F. J, Jr.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1940 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Motion of the two-control airplane in rectilinear flight after initial disturbances with introduction of controls following an exponential law / / by Alexander Klemin
| Motion of the two-control airplane in rectilinear flight after initial disturbances with introduction of controls following an exponential law / / by Alexander Klemin |
| Autore | Klemin Alexander <1888-1950, > |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1937 |
| Descrizione fisica | 1 online resource (30 pages, 10 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Stability of airplanes
Airplanes - Control Equations of motion |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910716726903321 |
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Klemin Alexander <1888-1950, >
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1937 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Preliminary report on the flat-top lift curve as a factor in control at low speed / / by Montgomery Knight and Millard J. Bamber
| Preliminary report on the flat-top lift curve as a factor in control at low speed / / by Montgomery Knight and Millard J. Bamber |
| Autore | Knight Montgomery |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1928 |
| Descrizione fisica | 1 online resource (10 pages, 5 unnumbered pages) : illustrations |
| Collana | Technical notes / National Advisory Committee for Aeronautics |
| Soggetto topico |
Aerofoils - Testing
Lift (Aerodynamics) - Speed Airplanes - Control |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910713657203321 |
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Knight Montgomery
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1928 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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Preliminary stability and control tests in the NACA free-flight wind tunnel and correlation with full-scale flight tests / / by Joseph A. Shortal and Clatyon J. Osterhout
| Preliminary stability and control tests in the NACA free-flight wind tunnel and correlation with full-scale flight tests / / by Joseph A. Shortal and Clatyon J. Osterhout |
| Autore | Shortal Joseph Adams <1908-> |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 |
| Descrizione fisica | 1 online resource (19 pages, 10 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Control
Stability of airplanes Wind tunnel testing |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717251403321 |
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Shortal Joseph Adams <1908->
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 | ||
| 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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Stability and control of aircraft systems : introduction to classical feedback control / / Roy Langton
| Stability and control of aircraft systems : 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 | 629.132/36 |
| Collana | Aerospace series |
| Soggetto topico |
Stability of airplanes
Airplanes - Control |
| ISBN |
9786610721177
9780470058480 047005848X 9781280721175 1280721170 9780470058497 0470058498 |
| 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-9911018817603321 |
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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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The theoretical lateral motions of an automatically controlled airplane subjected to a yawing-moment disturbance / / by Frederick H. Imlay
| The theoretical lateral motions of an automatically controlled airplane subjected to a yawing-moment disturbance / / by Frederick H. Imlay |
| Autore | Imlay Frederick H. |
| Pubbl/distr/stampa | Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 |
| Descrizione fisica | 1 online resource (16 pages, 7 unnumbered pages) : illustrations |
| Collana | Technical note / National Advisory Committee for Aeronautics |
| Soggetto topico |
Airplanes - Control
Automatic pilot (Airplanes) Stability of airplanes Yawing (Aerodynamics) |
| Formato | Materiale a stampa |
| Livello bibliografico | Monografia |
| Lingua di pubblicazione | eng |
| Record Nr. | UNINA-9910717251603321 |
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Imlay Frederick H.
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| Washington, [D.C.] : , : National Advisory Committee for Aeronautics, , 1941 | ||
| Materiale a stampa | ||
| Lo trovi qui: Univ. Federico II | ||
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