Guidance and Control of Homing Missiles (Paperback)

Bulent Ozkan

Editorial: LAP Lambert Academic Publishing, 2016
ISBN 10: 3847309617 / ISBN 13: 9783847309611
Nuevos / Paperback / Cantidad disponible: 0
Librería: The Book Depository EURO (London, Reino Unido)
Disponible en otras librerías
Ver todos  los ejemplares de este libro

Sobre el libro

Lamentablemente este ejemplar en específico ya no está disponible. A continuación, le mostramos una lista de copias similares.

Descripción:

Language: English . Brand New Book. Homing missiles have gained wide popularity in the field of guidance and control regarding the short and medium range purposes in recent years. In this study, the three-dimensional formulation of the Proportional Navigation Guidance (PNG) law is done. Another contribution of this study is the derivation of the Linear Homing Guidance (LHG) and the Parabolic Homing Guidance (PHG) laws. Then, all these three methods are implemented on both the considered missile model for the uncanted and canted tail wing configurations, and a generic single-body missile model. Also, the acceleration, rate and angular autopilots are designed in order to realize the guidance commands generated by these guidance laws on the considered missile models. Finally, the overall guidance and control models are constructed by integrating the obtained models and then numerous computer simulations are carried out to test the performance of the system in different scenarios. N° de ref. de la librería KNV9783847309611

Sobre este título:

Reseña del editor: Homing missiles have gained wide popularity in the field of guidance and control regarding the short and medium range purposes in recent years. In this study, the three-dimensional formulation of the Proportional Navigation Guidance (PNG) law is done. Another contribution of this study is the derivation of the Linear Homing Guidance (LHG) and the Parabolic Homing Guidance (PHG) laws. Then, all these three methods are implemented on both the considered missile model for the uncanted and canted tail wing configurations, and a generic single-body missile model. Also, the acceleration, rate and angular autopilots are designed in order to realize the guidance commands generated by these guidance laws on the considered missile models. Finally, the overall guidance and control models are constructed by integrating the obtained models and then numerous computer simulations are carried out to test the performance of the system in different scenarios.

"Sobre este título" puede pertenecer a otra edición de este libro.

Detalles bibliográficos

Título: Guidance and Control of Homing Missiles (...
Editorial: LAP Lambert Academic Publishing
Año de publicación: 2016
Encuadernación: Paperback
Condición del libro: New
Edición: Aufl.

Los mejores resultados en AbeBooks

1.

Bulent Ozkan (author)
Publicado por Omniscriptum Gmbh & Co. Kg. 2011-12-21 (2011)
ISBN 10: 3847309617 ISBN 13: 9783847309611
Nuevo paperback Cantidad disponible: > 20
Librería
Blackwell's
(Oxford, OX, Reino Unido)

Descripción Omniscriptum Gmbh & Co. Kg. 2011-12-21, 2011. paperback. Condición: New. Nº de ref. del artículo: 9783847309611

Más información sobre este vendedor | Contactar al vendedor

Comprar nuevo
EUR 71,94
Convertir moneda

Añadir al carrito

Gastos de envío: EUR 5,46
De Reino Unido a Estados Unidos de America
Destinos, gastos y plazos de envío

2.

Ozkan, Bulent
Publicado por LAP Lambert Academic Publishing (2011)
ISBN 10: 3847309617 ISBN 13: 9783847309611
Nuevo Cantidad disponible: > 20
Impresión bajo demanda
Librería
Books2Anywhere
(Fairford, GLOS, Reino Unido)

Descripción LAP Lambert Academic Publishing, 2011. PAP. Condición: New. New Book. Delivered from our UK warehouse in 4 to 14 business days. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. Nº de ref. del artículo: LQ-9783847309611

Más información sobre este vendedor | Contactar al vendedor

Comprar nuevo
EUR 76,38
Convertir moneda

Añadir al carrito

Gastos de envío: EUR 5,48
De Reino Unido a Estados Unidos de America
Destinos, gastos y plazos de envío

3.

Bulent Ozkan
Publicado por LAP Lambert Academic Publishing Aug 2016 (2016)
ISBN 10: 3847309617 ISBN 13: 9783847309611
Nuevo Taschenbuch Cantidad disponible: 1
Librería
Rheinberg-Buch
(Bergisch Gladbach, Alemania)

Descripción LAP Lambert Academic Publishing Aug 2016, 2016. Taschenbuch. Condición: Neu. Neuware - Homing missiles have gained wide popularity in the field of guidance and control regarding the short and medium range purposes in recent years. In this study, the three-dimensional formulation of the Proportional Navigation Guidance (PNG) law is done. Another contribution of this study is the derivation of the Linear Homing Guidance (LHG) and the Parabolic Homing Guidance (PHG) laws. Then, all these three methods are implemented on both the considered missile model for the uncanted and canted tail wing configurations, and a generic single-body missile model. Also, the acceleration, rate and angular autopilots are designed in order to realize the guidance commands generated by these guidance laws on the considered missile models. Finally, the overall guidance and control models are constructed by integrating the obtained models and then numerous computer simulations are carried out to test the performance of the system in different scenarios. 236 pp. Englisch. Nº de ref. del artículo: 9783847309611

Más información sobre este vendedor | Contactar al vendedor

Comprar nuevo
EUR 79,00
Convertir moneda

Añadir al carrito

Gastos de envío: EUR 17,13
De Alemania a Estados Unidos de America
Destinos, gastos y plazos de envío

4.

Bulent Ozkan
Publicado por LAP Lambert Academic Publishing Aug 2016 (2016)
ISBN 10: 3847309617 ISBN 13: 9783847309611
Nuevo Taschenbuch Cantidad disponible: 1
Impresión bajo demanda
Librería
AHA-BUCH GmbH
(Einbeck, Alemania)

Descripción LAP Lambert Academic Publishing Aug 2016, 2016. Taschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Neuware - Homing missiles have gained wide popularity in the field of guidance and control regarding the short and medium range purposes in recent years. In this study, the three-dimensional formulation of the Proportional Navigation Guidance (PNG) law is done. Another contribution of this study is the derivation of the Linear Homing Guidance (LHG) and the Parabolic Homing Guidance (PHG) laws. Then, all these three methods are implemented on both the considered missile model for the uncanted and canted tail wing configurations, and a generic single-body missile model. Also, the acceleration, rate and angular autopilots are designed in order to realize the guidance commands generated by these guidance laws on the considered missile models. Finally, the overall guidance and control models are constructed by integrating the obtained models and then numerous computer simulations are carried out to test the performance of the system in different scenarios. 236 pp. Englisch. Nº de ref. del artículo: 9783847309611

Más información sobre este vendedor | Contactar al vendedor

Comprar nuevo
EUR 79,00
Convertir moneda

Añadir al carrito

Gastos de envío: EUR 34,50
De Alemania a Estados Unidos de America
Destinos, gastos y plazos de envío

5.

Bulent Ozkan
Publicado por LAP Lambert Academic Publishing Aug 2016 (2016)
ISBN 10: 3847309617 ISBN 13: 9783847309611
Nuevo Taschenbuch Cantidad disponible: 1
Librería
BuchWeltWeit Inh. Ludwig Meier e.K.
(Bergisch Gladbach, Alemania)

Descripción LAP Lambert Academic Publishing Aug 2016, 2016. Taschenbuch. Condición: Neu. Neuware - Homing missiles have gained wide popularity in the field of guidance and control regarding the short and medium range purposes in recent years. In this study, the three-dimensional formulation of the Proportional Navigation Guidance (PNG) law is done. Another contribution of this study is the derivation of the Linear Homing Guidance (LHG) and the Parabolic Homing Guidance (PHG) laws. Then, all these three methods are implemented on both the considered missile model for the uncanted and canted tail wing configurations, and a generic single-body missile model. Also, the acceleration, rate and angular autopilots are designed in order to realize the guidance commands generated by these guidance laws on the considered missile models. Finally, the overall guidance and control models are constructed by integrating the obtained models and then numerous computer simulations are carried out to test the performance of the system in different scenarios. 236 pp. Englisch. Nº de ref. del artículo: 9783847309611

Más información sobre este vendedor | Contactar al vendedor

Comprar nuevo
EUR 79,00
Convertir moneda

Añadir al carrito

Gastos de envío: EUR 17,13
De Alemania a Estados Unidos de America
Destinos, gastos y plazos de envío

6.

Ozkan, Bulent
Publicado por LAP Lambert Academic Publishing (2017)
ISBN 10: 3847309617 ISBN 13: 9783847309611
Nuevo Paperback Cantidad disponible: 10
Impresión bajo demanda
Librería
Ria Christie Collections
(Uxbridge, Reino Unido)

Descripción LAP Lambert Academic Publishing, 2017. Paperback. Condición: New. PRINT ON DEMAND Book; New; Publication Year 2017; Not Signed; Fast Shipping from the UK. No. book. Nº de ref. del artículo: ria9783847309611_lsuk

Más información sobre este vendedor | Contactar al vendedor

Comprar nuevo
EUR 80,02
Convertir moneda

Añadir al carrito

Gastos de envío: EUR 4,24
De Reino Unido a Estados Unidos de America
Destinos, gastos y plazos de envío

7.

Ozkan, Bulent
Publicado por LAP Lambert Academic Publishing (2011)
ISBN 10: 3847309617 ISBN 13: 9783847309611
Nuevo Cantidad disponible: > 20
Impresión bajo demanda
Librería
Paperbackshop-US
(Wood Dale, IL, Estados Unidos de America)

Descripción LAP Lambert Academic Publishing, 2011. PAP. Condición: New. New Book. Shipped from UKs. THIS BOOK IS PRINTED ON DEMAND. Established seller since 2000. Nº de ref. del artículo: LQ-9783847309611

Más información sobre este vendedor | Contactar al vendedor

Comprar nuevo
EUR 89,48
Convertir moneda

Añadir al carrito

Gastos de envío: GRATIS
A Estados Unidos de America
Destinos, gastos y plazos de envío

8.

Bulent Ozkan
Publicado por LAP LAMBERT Academic Publishing (2011)
ISBN 10: 3847309617 ISBN 13: 9783847309611
Antiguo o usado Paperback Cantidad disponible: 1
Librería
Ergodebooks
(RICHMOND, TX, Estados Unidos de America)

Descripción LAP LAMBERT Academic Publishing, 2011. Paperback. Condición: Used: Good. Nº de ref. del artículo: SONG3847309617

Más información sobre este vendedor | Contactar al vendedor

Comprar usado
EUR 99,55
Convertir moneda

Añadir al carrito

Gastos de envío: GRATIS
A Estados Unidos de America
Destinos, gastos y plazos de envío

9.

Bulent Ozkan
Publicado por LAP Lambert Academic Publishing, Germany (2016)
ISBN 10: 3847309617 ISBN 13: 9783847309611
Nuevo Paperback Cantidad disponible: 10
Impresión bajo demanda
Librería
The Book Depository EURO
(London, Reino Unido)

Descripción LAP Lambert Academic Publishing, Germany, 2016. Paperback. Condición: New. Aufl. Language: English . Brand New Book ***** Print on Demand *****.Homing missiles have gained wide popularity in the field of guidance and control regarding the short and medium range purposes in recent years. In this study, the three-dimensional formulation of the Proportional Navigation Guidance (PNG) law is done. Another contribution of this study is the derivation of the Linear Homing Guidance (LHG) and the Parabolic Homing Guidance (PHG) laws. Then, all these three methods are implemented on both the considered missile model for the uncanted and canted tail wing configurations, and a generic single-body missile model. Also, the acceleration, rate and angular autopilots are designed in order to realize the guidance commands generated by these guidance laws on the considered missile models. Finally, the overall guidance and control models are constructed by integrating the obtained models and then numerous computer simulations are carried out to test the performance of the system in different scenarios. Nº de ref. del artículo: AAV9783847309611

Más información sobre este vendedor | Contactar al vendedor

Comprar nuevo
EUR 113,77
Convertir moneda

Añadir al carrito

Gastos de envío: EUR 3,29
De Reino Unido a Estados Unidos de America
Destinos, gastos y plazos de envío

10.

Ozkan, Bulent
Publicado por LAP LAMBERT Academic Publishin (2019)
ISBN 10: 3847309617 ISBN 13: 9783847309611
Nuevo Paperback Cantidad disponible: > 20
Impresión bajo demanda
Librería
Murray Media
(NORTH MIAMI BEACH, FL, Estados Unidos de America)

Descripción LAP LAMBERT Academic Publishin, 2019. Paperback. Condición: New. Never used! This item is printed on demand. Nº de ref. del artículo: 3847309617

Más información sobre este vendedor | Contactar al vendedor

Comprar nuevo
EUR 121,81
Convertir moneda

Añadir al carrito

Gastos de envío: GRATIS
A Estados Unidos de America
Destinos, gastos y plazos de envío

Existen otras 2 copia(s) de este libro

Ver todos los resultados de su búsqueda