Over the last few years, Unmanned Aerial Systems have proved to be highly efficient and capable of performing a wide range of applications, as well as development being more economical when compared to equivalent manned systems. This has resulted in the market for UAS increasing. An emerging role in this market is played by what is referred to as ‘HALE’ (High Altitude Long Endurance) UAV. This category of UAV presents itself as the ideal platform from which a wide range of different missions can be undertaken, both Military and Civilian, with versatility and a low maintenance cost. As a consequence, a growing number of Aerospace Companies from all over the world have shown interest in this innovative form of UAV. The purpose of this report is to present the design of a contemporary HALE UAV. The design process starts with the Conceptual phase, with the definition of the statistical analysis and the Matching Diagram. The results are optimized in the Preliminary phase by iterative procedures. Tools and methods used to size the aircraft design parameters are also presented. The research for this project was conducted at Imperial College of London and submitted to Politecnico of Turin.
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Over the last few years, Unmanned Aerial Systems have proved to be highly efficient and capable of performing a wide range of applications, as well as development being more economical when compared to equivalent manned systems. This has resulted in the market for UAS increasing. An emerging role in this market is played by what is referred to as ‘HALE’ (High Altitude Long Endurance) UAV. This category of UAV presents itself as the ideal platform from which a wide range of different missions can be undertaken, both Military and Civilian, with versatility and a low maintenance cost. As a consequence, a growing number of Aerospace Companies from all over the world have shown interest in this innovative form of UAV. The purpose of this report is to present the design of a contemporary HALE UAV. The design process starts with the Conceptual phase, with the definition of the statistical analysis and the Matching Diagram. The results are optimized in the Preliminary phase by iterative procedures. Tools and methods used to size the aircraft design parameters are also presented. The research for this project was conducted at Imperial College of London and submitted to Politecnico of Turin.
M.Sc. in Aerospace Engineering, Politecnico di Torino. Air Vehicle Engineer, Alenia Aermacchi S.p.A.. Varnavas Serghides is Senior Lecturer in Aerospace Vehicle Design, Dept. of Aeronautics, Imperial College, London. Sergio Chiesa is Full Professor in Aerospace System Design, Dept. of Mechanical and Aerospace Engineering, Politecnico di Torino.
Les informations fournies dans la section « A propos du livre » peuvent faire référence à une autre édition de ce titre.
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Taschenbuch. Etat : Neu. This item is printed on demand - it takes 3-4 days longer - Neuware -Over the last few years, Unmanned Aerial Systems have proved to be highly efficient and capable of performing a wide range of applications, as well as development being more economical when compared to equivalent manned systems. This has resulted in the market for UAS increasing. An emerging role in this market is played by what is referred to as HALE (High Altitude Long Endurance) UAV. This category of UAV presents itself as the ideal platform from which a wide range of different missions can be undertaken, both Military and Civilian, with versatility and a low maintenance cost. As a consequence, a growing number of Aerospace Companies from all over the world have shown interest in this innovative form of UAV. The purpose of this report is to present the design of a contemporary HALE UAV. The design process starts with the Conceptual phase, with the definition of the statistical analysis and the Matching Diagram. The results are optimized in the Preliminary phase by iterative procedures. Tools and methods used to size the aircraft design parameters are also presented. The research for this project was conducted at Imperial College of London and submitted to Politecnico of Turin. 232 pp. Englisch. N° de réf. du vendeur 9783845401317
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Etat : New. Dieser Artikel ist ein Print on Demand Artikel und wird nach Ihrer Bestellung fuer Sie gedruckt. Autor/Autorin: Sammartano DomenicoM.Sc. in Aerospace Engineering, Politecnico di Torino. Air Vehicle Engineer, Alenia Aermacchi S.p.A. Varnavas Serghides is Senior Lecturer in Aerospace Vehicle Design, Dept. of Aeronautics, Imperial College, Londo. N° de réf. du vendeur 5480302
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Taschenbuch. Etat : Neu. nach der Bestellung gedruckt Neuware - Printed after ordering - Over the last few years, Unmanned Aerial Systems have proved to be highly efficient and capable of performing a wide range of applications, as well as development being more economical when compared to equivalent manned systems. This has resulted in the market for UAS increasing. An emerging role in this market is played by what is referred to as HALE (High Altitude Long Endurance) UAV. This category of UAV presents itself as the ideal platform from which a wide range of different missions can be undertaken, both Military and Civilian, with versatility and a low maintenance cost. As a consequence, a growing number of Aerospace Companies from all over the world have shown interest in this innovative form of UAV. The purpose of this report is to present the design of a contemporary HALE UAV. The design process starts with the Conceptual phase, with the definition of the statistical analysis and the Matching Diagram. The results are optimized in the Preliminary phase by iterative procedures. Tools and methods used to size the aircraft design parameters are also presented. The research for this project was conducted at Imperial College of London and submitted to Politecnico of Turin. N° de réf. du vendeur 9783845401317
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Taschenbuch. Etat : Neu. Conceptual and Preliminary Design for a HALE UAV | Process, Tools, and Design Methodologies applied to High Altitude Long Endurance Unmanned Aerial Vehicle | Domenico Sammartano (u. a.) | Taschenbuch | Paperback | 232 S. | Englisch | 2015 | LAP Lambert Academic Publishing | EAN 9783845401317 | Verantwortliche Person für die EU: BoD - Books on Demand, In de Tarpen 42, 22848 Norderstedt, info[at]bod[dot]de | Anbieter: preigu. N° de réf. du vendeur 106481281
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Taschenbuch. Etat : Neu. This item is printed on demand - Print on Demand Titel. Neuware -Over the last few years, Unmanned Aerial Systems have proved to be highly efficient and capable of performing a wide range of applications, as well as development being more economical when compared to equivalent manned systems. This has resulted in the market for UAS increasing. An emerging role in this market is played by what is referred to as 'HALE' (High Altitude Long Endurance) UAV. This category of UAV presents itself as the ideal platform from which a wide range of different missions can be undertaken, both Military and Civilian, with versatility and a low maintenance cost. As a consequence, a growing number of Aerospace Companies from all over the world have shown interest in this innovative form of UAV. The purpose of this report is to present the design of a contemporary HALE UAV. The design process starts with the Conceptual phase, with the definition of the statistical analysis and the Matching Diagram. The results are optimized in the Preliminary phase by iterative procedures. Tools and methods used to size the aircraft design parameters are also presented. The research for this project was conducted at Imperial College of London and submitted to Politecnico of Turin.Books on Demand GmbH, Überseering 33, 22297 Hamburg 232 pp. Englisch. N° de réf. du vendeur 9783845401317
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