Detalles MARC
| 000 -Cabecera |
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| fixed length control field |
05104mm a2200493a 44500 |
| 001 - Número de control |
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| control field |
NM000552 |
| 003 - Identificador del Número de control |
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| control field |
AR-HaUTN |
| 005 - Fecha y hora de la última transacción |
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| control field |
20240917164006.0 |
| 007 - Campo fijo de descripción fija-Información general |
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| fixed length control field |
ta |
| 008 - Elementos de longitud fija-Información general |
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| fixed length control field |
98020sc. 1 ||||||||||||||000 | spa|| |
| 020 ## - ISBN |
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| ISBN |
0471506516 |
| 040 ## - Fuente de catalogación |
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| Agencia de catalogación original |
AR-HaUTN |
| Agencia que realiza la transcripción |
AR-HaUTN |
| 100 ## - Asiento principal-Nombre personal |
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| Nombre personal |
Blakelock, John H. |
| 9 (RLIN) |
3063 |
| 245 ## - Mención de título |
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| Título |
Automatic control of aircraft and missiles |
| Mención de responsabilidad |
John H. Blakelock |
| 250 ## - Mención de edición |
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| Edición |
2nd. ed. |
| 260 ## - Publicación y distribución |
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| Lugar de edición |
New York |
| Nombre del editor |
John Wiley |
| 300 ## - Descripción física |
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| Extensión |
xv, 646 p. |
| Otros detalles físicos |
gráficos |
| 500 ## - Nota general |
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| Nota general |
Indice alfabético, al final del libro |
| 504 ## - Nota de bibliografía, etc. |
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| Nota de bibliografía, etc. |
Referencias bibliográficas, al final de cada capítulo |
| 505 ## - Nota de contenido |
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| Título |
Longitudinal dynamics :<br/>Introduction. The meaning of velocoties in a moving axis system. Development of the equations of motion (Controls locked). Aircraft attitude with respect to the earth. Linearization and separation of the equations of motion. Longitudinal equations of motion. Derivation of equations for the longitudinal stability derivatives. Solution of the longitudinal equations (Stick fixed). Longitudinal transfer function for elevator displacement. Trasient response of the aircraft. Effect of variation of stability derivatives on aircraft performance. |
| 505 ## - Nota de contenido |
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| Título |
Longitudinal autopilots :<br/>Displacement autopilot. Pitch orientational control system. Acceleration control system. Gilde slope coupler and automatic flare control. Flight path stabilization. Vertical gyro as the basic attitude reference. Gyro stabilized platform as the basic attitude. Effects of nonlinearities |
| 505 ## - Nota de contenido |
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| Título |
Lateral dynamics :<br/>Lateral equations of motion. Derivation of equations for the lateral stability. Derivatives. Solution of lateral esquations (stick fixed). Lateral transfer function for rudder. Displacement. Lateral transfer function for aileron. Displacement. Approximate transfer functions. Transient response of the aircraft. Effect of stability derivative variation |
| 505 ## - Nota de contenido |
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| Título |
Lateral autopilots : <br/>Introduction. Damping of the dutch roll. Methods of obtaining coordination. Discussion of coordination techniques. Yaw orientational control system. Other lateral autopilot configurations. Turn compensation. Automatic lateral beam guidance. Nonlinear effects |
| 505 ## - Nota de contenido |
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| Título |
Inertial cross-coupling :<br/>Introduction. Effects of high roll rates. Determination of the aircraft parameters that affect stability. System for controlling an aircraft subject to inertial cross-coupling. Imprved system for controlling an aircraft subject to inertial cross-coupling |
| 505 ## - Nota de contenido |
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| Título |
Sel-fadaptive autopilots :<br/>Introduction. General philosophy of the self-adaptive control system. Sperry sepf-adaptive control system. Minneapolis-Honeywell self-adaptive control system. Mit model-reference adaptive control system for aircraft. MH-90 adaptive control system. Summary |
| 505 ## - Nota de contenido |
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| Título |
Missile control systems : <br/>Introduction. Rollstabilization. Control of aerodynamic missiles. transfer function for a ballistic-type missile. Vanguard control system(rigid missile). Alternate missile control system(rigid missile). Summary |
| 505 ## - Nota de contenido |
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| Título |
Guidance systems :<br/>Introduction. Proportional navigation guidance. Comparison of guidance system performance.. Bank-to turn missile guidance. Short/medium-range BTT missile. |
| 505 ## - Nota de contenido |
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| Título |
Integrated flight / Fire control system :<br/>Introduction. Director fire control system. Longitudinal flight control system. Lateral flight control system. Verification of lateral control system analysis. Velocity control system. Movable gun control. Gimbaled tracker desing. Tracking control laws (TCL). Discrete analysis. Simulation resuls. |
| 505 ## - Nota de contenido |
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| Título |
Multivariable control systems : <br/>Introduction. Multivariable desing without servo dynamics. Multivariable desing with servo dynamics. Multivariable desing of YOCS. Sumary. |
| 505 ## - Nota de contenido |
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| Título |
Structural flexibility :<br/>Introduction. Lagrange´s equation. Lagrange´s equation apllied to a system of lumped para meters. Mode shapes and frequencies. Normal coordinates. System transfer function, including body bending. The "Tail-WagsDog" Zero. Effects of propellant sloshing. Compensation required for body bending. Summary |
| 505 ## - Nota de contenido |
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| Título |
Application of statistical design principles :<br/>Introduction. Random processes. Mean-square error. Autocorrelation function. Cross-correlation function. Power spectral density. Application of statistical desing principles. Additional applications of stastical design principles. Summary |
| 505 ## - Nota de contenido |
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| Título |
Pilot modeling :<br/>Introduction. Crossover model. The paper pilot. Optimal pilot model. |
| 505 ## - Nota de contenido |
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| Título |
Review of vector analysis [Appendix A] : |
| 505 ## - Nota de contenido |
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| Título |
Some gyroscopic theory [Appendix B] |
| 505 ## - Nota de contenido |
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| Título |
Basic servo theory [Appendix C] |
| 505 ## - Nota de contenido |
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| Título |
Fundamental aerodynamic principles [Appendix D] |
| 505 ## - Nota de contenido |
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| Título |
Matrices [Appendix E] |
| 505 ## - Nota de contenido |
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| Título |
F94A and F15 longitudinal and lateral aerodynamic data [Appendix F] |
| 505 ## - Nota de contenido |
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| Título |
Wind axes [Appendix G] |
| 505 ## - Nota de contenido |
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| Título |
Digital simulation of transfer functions [Appendix H] |
| 505 ## - Nota de contenido |
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| Título |
Fire control problem [Appendix I] |
| 505 ## - Nota de contenido |
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| Título |
A1 and A4 gunsights [Appendix J] |
| 942 ## - Puntos de acceso adicionales KOHA (No-MARC) |
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| Tipo de item KOHA |
Libro |
| Source of classification or shelving scheme |
Universal Decimal Classification |
