ISBN: 9783330048607 - mathematical modeling of guided weapons for autopilot designing (5 resultados)

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  • Idioma: Inglés

    Editorial: LAP LAMBERT Academic Publishing, 2017

    3330048603 / 9783330048607

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    Librería: Revaluation Books, Exeter, Reino UnidoRevaluation Books

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    EUR 86,18

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    Paperback. Condición: Brand New. 92 pages. 8.66x5.91x0.21 inches. In Stock.

  • Idioma: Inglés

    Editorial: LAP LAMBERT Academic Publishing Mrz 2017, 2017

    3330048603 / 9783330048607

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    Librería: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, AlemaniaBuchWeltWeit Ludwig Meier e.K.

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    EUR 49,90

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    Taschenbuch. Condición: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Requirements for next generation guided weapons, particularly with respect to their capability to engage high speed, highly agile targets and achieve precision end-game trajectory has prompted a revision of the way in which the guidance and autopilot design is undertaken. This book considered the derivation of mathematical models for a missile autopilot for autopilot in State Space form. The basic model developed was highly nonlinear and is difficult to analyze analytically. Therefore Jacobian linearization technique was used to linear the model.The models developed are useful for further research on precision optimum guidance and control. The model will provide more accurate presentations of missile autopilot dynamics and can be used for adaptive and integrated guidance and control of agile missiles. 92 pp. Englisch.…

  • Idioma: Inglés

    Editorial: LAP LAMBERT Academic Publishing, 2017

    3330048603 / 9783330048607

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    Librería: AHA-BUCH GmbH, Einbeck, AlemaniaAHA-BUCH GmbH

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    EUR 49,90

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    Taschenbuch. Condición: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Requirements for next generation guided weapons, particularly with respect to their capability to engage high speed, highly agile targets and achieve precision end-game trajectory has prompted a revision of the way in which the guidance and autopilot design is undertaken. This book considered the derivation of mathematical models for a missile autopilot for autopilot in State Space form. The basic model developed was highly nonlinear and is difficult to analyze analytically. Therefore Jacobian linearization technique was used to linear the model.The models developed are useful for further research on precision optimum guidance and control. The model will provide more accurate presentations of missile autopilot dynamics and can be used for adaptive and integrated guidance and control of agile missiles.…

  • Idioma: Inglés

    Editorial: LAP LAMBERT Academic Publishing, 2017

    3330048603 / 9783330048607

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    Librería: moluna, Greven, Alemaniamoluna

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    EUR 41,71

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    Condición: New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Joshi PuneetEr. Puneet Joshi is pursuing his Ph.D. in Electrical Engineering, from G.B.P.U.A.T., Pantnagar,Uttarakhand,India. He received his M.Tech. degree in (Electrical Engineering) Electrical Energy Systems from G.B.P.U.A.T.,Pant.…

  • Idioma: Inglés

    Editorial: LAP LAMBERT Academic Publishing Mär 2017, 2017

    3330048603 / 9783330048607

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    Librería: buchversandmimpf2000, Emtmannsberg, BAYE, Alemaniabuchversandmimpf2000

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    EUR 49,90

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    Cantidad disponible: 1 disponible

    Taschenbuch. Condición: Neu. This item is printed on demand - Print on Demand Titel. Neuware -Requirements for next generation guided weapons, particularly with respect to their capability to engage high speed, highly agile targets and achieve precision end-game trajectory has prompted a revision of the way in which the guidance and autopilot design is undertaken. This book considered the derivation of mathematical models for a missile autopilot for autopilot in State Space form. The basic model developed was highly nonlinear and is difficult to analyze analytically. Therefore Jacobian linearization technique was used to linear the model.The models developed are useful for further research on precision optimum guidance and control. The model will provide more accurate presentations of missile autopilot dynamics and can be used for adaptive and integrated guidance and control of agile missiles.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 92 pp. Englisch.…