Modeling of complex systems : application to aeronautical dynamics / / Emmanuel Grunn, Anh Tuan Pham

• Autore: Grunn Emmanuel
• Pubblicazione: London ; ; Hoboken, New Jersey : , : ISTE : , : Wiley, , 2013; ©2013
• Descrizione fisica: 1 online resource (124 p.)
• Disciplina: 629.13230151
• Soggetto topico: Aerodynamics - Mathematics; System analysis - Mathematical models
• Altri autori: PhạmAnh Tuan (Engineer)
• Note generali: Description based upon print version of record.
• Nota di bibliografia: Includes bibliographical references and index.
• Nota di contenuto: Cover; Title Page; Table of Contents; Introduction; Chapter 1. 0D Analytical Modeling of Airplane Motions; 1.1. References: axis systems on use; 1.1.1. Galilean reference: R0; 1.1.2. Airplane reference: RB (body) also called "linked reference"; 1.1.3. Resultant angular velocity; 1.2. Equations of motion of the airplane; 1.2.1. Expression of Newton's principle; 1.2.2. Expression of the dynamic momentum; 1.3. Description of external forces and torques; 1.3.1. Aerodynamic forces and torques; 1.3.2. Sign rules; 1.4. Description of aerodynamic coefficients; 1.4.1. Drag coefficient: Cx ; 1.4.2. Side lift coefficient: CY1.4.3. Vertical lift due to attack angle: CZα; 1.4.4. Lift due to pitch angular velocity: CZq; 1.4.5. Roll coefficients (due to β, δl , p); 1.4.6. Pitch coefficients (due to α, δm , q , static curvature); 1.4.7. Yaw coefficients (due to β, δn, r); 1.5. Aerodynamic data of a supersonic airliner for valuation of the software; 1.6. Horizontal flight as an initial condition; 1.7. Effect of gravitational forces; 1.8 calculation of the trajectory of the airplane in open space; 1.9. Validation by comparison with ONERA Concorde data ; 1.10. Definitions of aerodynamic coefficients and derivatives 1.10.1.1.10.1. Aerodynamic coefficients; 1.10.2. Total lift coefficient; 1.10.3. Drag characteristics: (dimensionless); 1.10.4. Side lift coefficient: CY (dimensionless); 1.10.5. Roll coefficients; 1.10.6. Pitch coefficients; 1.10.7. Yaw coefficients; Chapter 2. Design and Optimization of anUnmanned Aerial Vehicle (UAV); 2.1. General design of the drone; 2.2. Weight estimation; 2.3. Size estimation; 2.4. Mass and inertia evaluation; 2.4.1. Mass evaluation; 2.4.2. Measurement of the roll inertia (A) ; 2.4.3. Measurement of pitch inertia (B)2.4.4. Measurement of yaw inertia (C); 2.5. Convergence toward the target; Chapter 3. Organization of the Auto-Pilot; 3.1. Position of the drone in open space; 3.2. The Dog Law; 3.3. Flight tests; 3.4. Altitude control system; 3.5. Altitude measurement on an actual drone; Bibliography; Index
• Sommario/riassunto: In the field of aeronautical dynamics, this book offers readers a design tool which enables them to solve the different problems that can occur during the planning stage of a private project. The authors present a system for the modeling, design and calculation of the flying qualities of airplanes and drones, with a complete mathematical model by Matlab/Simulink. As such, this book may be useful for design engineers as well as for keen airplane amateurs.The authors expound the various phases involved in the design process of an airplane, starting with the formulation of a design tool, un
• Titolo autorizzato: Modeling of complex systems
• ISBN: 1-118-57986-0; 1-118-57997-6; 1-118-58007-9
• Formato: Materiale a stampa
• Livello bibliografico: Monografia
• Lingua di pubblicazione: Inglese
• Record Nr.: 9910820286703321
• Lo trovi qui: Univ. Federico II
• Serie: Focus series (London, England)