Radio remote-control and telemetry and their application to missiles /

Radio Remote-Control and Telemetry and Their Application to Missiles.

Detalles Bibliográficos
Clasificación:Libro Electrónico
Autor principal: Marcus, Jean (Autor)
Otros Autores: Hawkes, P. W. (Traductor)
Formato: Electrónico eBook
Idioma:Inglés
Publicado: Oxford ; New York : Pergamon Press, [1966]
Edición:First English edition /
Temas:
Space vehicles > Command control systems.
Aerospace telemetry.
Information theory.
Space vehicles > Control systems.
V�ehicules spatiaux > Syst�emes de commande.
Th�eorie de l'information.
TECHNOLOGY & ENGINEERING > Military Science.
Space vehicles > Control systems
Aerospace telemetry
Information theory
Space vehicles > Command control systems
Acceso en línea:Texto completo
Tabla de Contenidos:
  • Cover image; Title page; Table of Contents; Copyright; PREFACE; Chapter I: GENERAL REMARKS; I.1 THE DIFFERENT TYPES OF SPECIAL MISSILE; I.2 THE MISSILE GUIDANCE PROBLEM; I.3 GENERAL REMARKS ABOUT THE REQUIREMENTS OF THE ELECTRICAL EQUIPMENT; I.4 THE SOURCES OF ERROR AND THEIR EFFECTS; I.5 LIMITATIONS OF WEIGHT AND BULK; Chapter II: THE DIFFERENT TYPES OF MODULATION; II. 1 AMPLITUDE MODULATION (AM); II. 3 PULSE MODULATION; II. 4 CODED MODULATION (PCM); APPENDIX-GAUSSIAN PULSES(100); Chapter III: INFORMATION AND CODING; III. 1 THE NATURE OF THE INFORMATION; III. 2 A MEASURE OF THE INFORMATION.
  • III. 3 THE CAPACITY OF A TRANSMISSION CHANNELIII. 4 APPLICATIONS TO THE CASE OF MULTIPLEX LINKS; III. 5 SOME EXAMPLES OF THE APPLICATION OF THE CONCEPT OF INFORMATION EFFICIENCY; III. 6 SENSIBLE USE OF INFORMATION FOR LONG-RANGE LINKS; III. 7 CODING; III. 8 METHODS OF CODING AND DECODING; APPENDIX
  • REASONS FOR CHOOSING THE BINARY SYSTEM; Chapter IV: LIMITATIONS ON INFORMATION; IV. 1 THE PHENOMENON OF NOISE; IV. 2 INTERFERENCE AND JAMMING PHENOMENA; IV. 3 ERRORS AND THRESHOLDS OF MEASUREMENT; IV. 4 DISTORTION DUE TO NON-LINEARITY; Chapter V: FIELD PROPAGATION AND AERIALS ON MISSILES.
  • V.1 GENERAL REMARKSV. 2 LOW ALTITUDE MISSILES; V.3 MISSILES TRAVELLING AT GREAT ALTITUDES; V.4 VARIATIONS IN THE GAIN OF AERIALS; V.5 THE PROBLEM OF ATTACHING AERIALS TO A MISSILE; V.6 PROCEDURES WHICH ARE EMPLOYED TO INCREASE THE EQUIVALENT AREA OF MISSILES STATICALLY; V.7 LINKS WITH DIVERSITY; Chapter VI: RADIO LINKS FOR REMOTE-CONTROL AND TELEMETRY EQUIPMENT, REGARDED AS MULTIPLEX SYSTEMS; VI. 1 MULTIPLEXING BY DISTRIBUTION OVER FREQUENCY; VI. 2 MULTIPLEX SYSTEMS WITH TEMPORAL DISTRIBUTION; VI. 3 THE THRESHOLD RANGE OF A RADIO LINK.
  • VI. 4 COMPARISON OF DIFFERENT TYPES OF MODULATION AND MULTIPLEXINGChapter VII: THE GUIDANCE OF MISSILES BY RADIO REMOTE-CONTROL; VII. 1 THE POSITION OF REMOTE-CONTROL IN THE NAVIGATIONAL SYSTEM; VII. 2 PILOTING BY REMOTE-CONTROL; VII. 3 DECODING THE REMOTE-CONTROL COMMANDS; VII. 4 EXAMPLES OF RADIO REMOTE-CONTROL SYSTEMS; VII. 5 OPTIMUM FILTERING FOR MISSILE GUIDANCE; Chapter VIII: RADIO TELEMETRY EQUIPMENT; VIII. 1 GENERAL REMARKS; VIII. 2 FEATURES PECULIAR TO TELEMETRY: THE TRANSDUCERS; VIII. 3 NON-LINEARITY IN TRANSDUCERS(34); VIII. 4 THE CONVERTERS; VIII. 5 SOME PRACTICAL EXAMPLES.
  • VIII. 6 RECOVERY OF THE DATAChapter IX: CONCLUSION; APPENDIX: STANDARDS FOR TELEMETRY; BIBLIOGRAPHY; INDEX.

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