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Optimal External Configuration Design of Missiles: Multidisciplinary Conceptual Design of Tactical Missiles Based on Genetic Algorithm - Softcover
Synopsis
The main area of emphasis in the work is to investigate the methods and technology for aerodynamic configuration sizing of missiles and to develop a software platform (EXCON) in MATLAB environment as a design tool which has an ability of optimizing the external configuration of missiles for a set of flight requirements. In this multidisciplinary optimization (MDO) process, the external geometry candidates are graded according to their flight performances to discover an optimum solution. All of the flight performance data are obtained by running a flight simulation which uses Missile DATCOM as the aerodynamic coefficient prediction software package. In order to solve the resulting multi-objective optimization problem with a set of constraint of linear and nonlinear nature, improved evolutionary methods are applied. Also, a case study, the reconfiguration problem of an anti-ship cruise missile, is presented to demonstrate the accuracy and feasibility of the conceptual design tool developed. The book is suitable for engineers who are involved in the system-level preliminary design of the cruise missiles or in rapid prototyping of aircrafts using advanced MDO techniques.
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About the Author
Çağatay Tanıl is a Senior Design Engineer in Roketsan Missile Industries Inc. He has been involved in control systems, modeling & simulation and mission planning in aerospace applications. He obtained his BS and MS degrees from Mechanical Engineering Department of Middle East Technical University (METU). His e-mail address is ctanil@roketsan.com.tr
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Optimal External Configuration Design of Missiles
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LAP LAMBERT Academic Publishing Sep 2011, 2011
ISBN 10: 384650582X
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Taschenbuch. Condition: Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -The main area of emphasis in the work is to investigate the methods and technology for aerodynamic configuration sizing of missiles and to develop a software platform (EXCON) in MATLAB environment as a design tool which has an ability of optimizing the external configuration of missiles for a set of flight requirements. In this multidisciplinary optimization (MDO) process, the external geometry candidates are graded according to their flight performances to discover an optimum solution. All of the flight performance data are obtained by running a flight simulation which uses Missile DATCOM as the aerodynamic coefficient prediction software package. In order to solve the resulting multi-objective optimization problem with a set of constraint of linear and nonlinear nature, improved evolutionary methods are applied. Also, a case study, the reconfiguration problem of an anti-ship cruise missile, is presented to demonstrate the accuracy and feasibility of the conceptual design tool developed. The book is suitable for engineers who are involved in the system-level preliminary design of the cruise missiles or in rapid prototyping of aircrafts using advanced MDO techniques. 168 pp. Englisch. Seller Inventory # 9783846505823
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Optimal External Configuration Design of Missiles
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Optimal External Configuration Design of Missiles
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Optimal External Configuration Design of Missiles
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Optimal External Configuration Design of Missiles | Multidisciplinary Conceptual Design of Tactical Missiles Based on Genetic Algorithm
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Taschenbuch. Condition: Neu. Optimal External Configuration Design of Missiles | Multidisciplinary Conceptual Design of Tactical Missiles Based on Genetic Algorithm | Ça¿atay Tan¿l (u. a.) | Taschenbuch | 168 S. | Englisch | 2011 | LAP LAMBERT Academic Publishing | EAN 9783846505823 | Verantwortliche Person für die EU: preigu GmbH & Co. KG, Lengericher Landstr. 19, 49078 Osnabrück, mail[at]preigu[dot]de | Anbieter: preigu. Seller Inventory # 106793862
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Optimal External Configuration Design of Missiles
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LAP LAMBERT Academic Publishing Sep 2011, 2011
ISBN 10: 384650582X
ISBN 13: 9783846505823
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Taschenbuch. Condition: Neu. This item is printed on demand - Print on Demand Titel. Neuware -The main area of emphasis in the work is to investigate the methods and technology for aerodynamic configuration sizing of missiles and to develop a software platform (EXCON) in MATLAB environment as a design tool which has an ability of optimizing the external configuration of missiles for a set of flight requirements. In this multidisciplinary optimization (MDO) process, the external geometry candidates are graded according to their flight performances to discover an optimum solution. All of the flight performance data are obtained by running a flight simulation which uses Missile DATCOM as the aerodynamic coefficient prediction software package. In order to solve the resulting multi-objective optimization problem with a set of constraint of linear and nonlinear nature, improved evolutionary methods are applied. Also, a case study, the reconfiguration problem of an anti-ship cruise missile, is presented to demonstrate the accuracy and feasibility of the conceptual design tool developed. The book is suitable for engineers who are involved in the system-level preliminary design of the cruise missiles or in rapid prototyping of aircrafts using advanced MDO techniques.VDM Verlag, Dudweiler Landstraße 99, 66123 Saarbrücken 168 pp. Englisch. Seller Inventory # 9783846505823
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Optimal External Configuration Design of Missiles : Multidisciplinary Conceptual Design of Tactical Missiles Based on Genetic Algorithm
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ISBN 10: 384650582X
ISBN 13: 9783846505823
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Taschenbuch. Condition: Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - The main area of emphasis in the work is to investigate the methods and technology for aerodynamic configuration sizing of missiles and to develop a software platform (EXCON) in MATLAB environment as a design tool which has an ability of optimizing the external configuration of missiles for a set of flight requirements. In this multidisciplinary optimization (MDO) process, the external geometry candidates are graded according to their flight performances to discover an optimum solution. All of the flight performance data are obtained by running a flight simulation which uses Missile DATCOM as the aerodynamic coefficient prediction software package. In order to solve the resulting multi-objective optimization problem with a set of constraint of linear and nonlinear nature, improved evolutionary methods are applied. Also, a case study, the reconfiguration problem of an anti-ship cruise missile, is presented to demonstrate the accuracy and feasibility of the conceptual design tool developed. The book is suitable for engineers who are involved in the system-level preliminary design of the cruise missiles or in rapid prototyping of aircrafts using advanced MDO techniques. Seller Inventory # 9783846505823
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Optimal External Configuration Design of Missiles: Multidisciplinary Conceptual Design of Tactical Missiles Based on Genetic Algorithm
Published by
LAP LAMBERT Academic Publishing, 2011
ISBN 10: 384650582X
ISBN 13: 9783846505823
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