9783330048607 - Mathematical Modeling of Guided Weapons for Autopilot Designing by Joshi, Puneet; Joshi, Medha (6 results)
- Softcover
Seller: Revaluation Books, Exeter, , United KingdomRevaluation Books
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Paperback. Condition: Brand New. 92 pages. 8.66x5.91x0.21 inches. In Stock.
- Softcover
Seller: preigu, Osnabrück, Germanypreigu
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Taschenbuch. Condition: Neu. Mathematical Modeling of Guided Weapons for Autopilot Designing | Puneet Joshi (u. a.) | Taschenbuch | 92 S. | Englisch | 2017 | LAP LAMBERT Academic Publishing | EAN 9783330048607 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]…de | Anbieter: preigu.
Language: English
Published by LAP LAMBERT Academic Publishing Mrz 2017 2017
- Softcover
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Seller: BuchWeltWeit Ludwig Meier e.K., Bergisch Gladbach, , GermanyBuchWeltWeit Ludwig Meier e.K.
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Taschenbuch. Condition: 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 guid…ance 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.
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Seller: moluna, Greven, , Germanymoluna
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Condition: 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.
Language: English
Published by LAP LAMBERT Academic Publishing Mär 2017 2017
- Softcover
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Seller: buchversandmimpf2000, Emtmannsberg, BAYE, Germanybuchversandmimpf2000
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Taschenbuch. Condition: 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.
- Softcover
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Seller: AHA-BUCH GmbH, Einbeck, GermanyAHA-BUCH GmbH
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Taschenbuch. Condition: 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.
