LEADER 04620nam 2200661 450 001 9910820286703321 005 20230927014048.0 010 $a1-118-57986-0 010 $a1-118-57997-6 010 $a1-118-58007-9 035 $a(CKB)2670000000494157 035 $a(EBL)1575624 035 $a(SSID)ssj0001173834 035 $a(PQKBManifestationID)11763802 035 $a(PQKBTitleCode)TC0001173834 035 $a(PQKBWorkID)11107460 035 $a(PQKB)10588760 035 $a(MiAaPQ)EBC1575624 035 $a(Au-PeEL)EBL1575624 035 $a(CaPaEBR)ebr10814678 035 $a(CaONFJC)MIL550367 035 $a(OCoLC)865333403 035 $a(EXLCZ)992670000000494157 100 $a20131219d2013 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aModeling of complex systems $eapplication to aeronautical dynamics /$fEmmanuel Grunn, Anh Tuan Pham 210 1$aLondon ;$aHoboken, New Jersey :$cISTE :$cWiley,$d2013. 210 4$dİ2013 215 $a1 online resource (124 p.) 225 0$aAutomation-control and industrial engineering series 300 $aDescription based upon print version of record. 311 $a1-84821-448-0 320 $aIncludes bibliographical references and index. 327 $aCover; 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 327 $a1.4.2. Side lift coefficient: CY1.4.3. Vertical lift due to attack angle: CZ?; 1.4.4. Lift due to pitch angular velocity: CZq; 1.4.5. Roll coefficients (due to ?, ?l , p); 1.4.6. Pitch coefficients (due to ?, ?m , q , static curvature); 1.4.7. Yaw coefficients (due to ?, ?n, 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 327 $a1.10. 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) 327 $a2.4.3. 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 330 $aIn the field of aeronautical dynamics, this book offers readers a design tool which enables them to solve the different problems that can occur during the planning stage of a private project. The authors present a system for the modeling, design and calculation of the flying qualities of airplanes and drones, with a complete mathematical model by Matlab/Simulink. As such, this book may be useful for design engineers as well as for keen airplane amateurs.The authors expound the various phases involved in the design process of an airplane, starting with the formulation of a design tool, un 410 0$aFocus series (London, England) 606 $aAerodynamics$xMathematics 606 $aSystem analysis$xMathematical models 615 0$aAerodynamics$xMathematics. 615 0$aSystem analysis$xMathematical models. 676 $a629.13230151 700 $aGrunn$b Emmanuel$01710906 701 $aPha?m$b Anh Tuan$c(Engineer)$01710907 712 02$aJohn Wiley & Sons, 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910820286703321 996 $aModeling of complex systems$94101849 997 $aUNINA