LEADER 05537nam 2200721 a 450 001 9910784357203321 005 20231005152211.0 010 $a1-281-02927-0 010 $a9786611029272 010 $a0-08-055036-3 035 $a(CKB)1000000000350072 035 $a(EBL)311429 035 $a(OCoLC)476098506 035 $a(SSID)ssj0000155995 035 $a(PQKBManifestationID)11156778 035 $a(PQKBTitleCode)TC0000155995 035 $a(PQKBWorkID)10123160 035 $a(PQKB)11219271 035 $a(MiAaPQ)EBC311429 035 $a(Au-PeEL)EBL311429 035 $a(CaPaEBR)ebr10188597 035 $a(CaONFJC)MIL102927 035 $a(OCoLC)1398231511 035 $a(OCoLC-P)1398231511 035 $a(CaSebORM)9780750669276 035 $a(EXLCZ)991000000000350072 100 $a20070427d2007 uy 0 101 0 $aeng 135 $aur|n|---||||| 181 $ctxt 182 $cc 183 $acr 200 10$aFlight dynamics principles$b[electronic resource] $e[a linear systems approach to aircraft stability and control] /$fM.V. Cook 205 $a2nd ed. 210 $aOxford [UK] ;$aBurlington, MA $cButterworth-Heinemann/Elsevier$d2007 215 $a1 online resource (491 p.) 225 1 $aElsevier aerospace engineering series 300 $aDescription based upon print version of record. 311 $a0-7506-6927-6 327 $aFront cover; Flight Dynamics Principles; Copyright page; Contents; Preface to the first edition; Preface to the second edition; Acknowledgements; Nomenclature; Chapter 1. Introduction; 1.1 Overview; 1.2 Flying and handling qualities; 1.3 General considerations; 1.4 Aircraft equations of motion; 1.5 Aerodynamics; 1.6 Computers; 1.7 Summary; References; Chapter 2. Systems of axes and notation; 2.1 Earth axes; 2.2 Aircraft body fixed axes; 2.3 Euler angles and aircraft attitude; 2.4 Axes transformations; 2.5 Aircraft reference geometry; 2.6 Controls notation; 2.7 Aerodynamic reference centres 327 $aReferencesProblems; Chapter 3. Static equilibrium and trim; 3.1 Trim equilibrium; 3.2 The pitching moment equation; 3.3 Longitudinal static stability; 3.4 Lateral static stability; 3.5 Directional static stability; 3.6 Calculation of aircraft trim condition; References; Problems; Chapter 4. The equations of motion; 4.1 The equations of motion of a rigid symmetric aircraft; 4.2 The linearised equations of motion; 4.3 The decoupled equations of motion; 4.4 Alternative forms of the equations of motion; References; Problems; Chapter 5. The solution of the equations of motion 327 $a5.1 Methods of solution5.2 Cramer's rule; 5.3 Aircraft response transfer functions; 5.4 Response to controls; 5.5 Acceleration response transfer functions; 5.6 The state space method; 5.7 State space model augmentation; References; Problems; Chapter 6. Longitudinal dynamics; 6.1 Response to controls; 6.2 The dynamic stability modes; 6.3 Reduced order models; 6.4 Frequency response; 6.5 Flying and handling qualities; 6.6 Mode excitation; References; Problems; Chapter 7. Lateral-directional dynamics; 7.1 Response to controls; 7.2 The dynamic stability modes; 7.3 Reduced order models 327 $a7.4 Frequency response7.5 Flying and handling qualities; 7.6 Mode excitation; References; Problems; Chapter 8. Manoeuvrability; 8.1 Introduction; 8.2 The steady pull-up manoeuvre; 8.3 The pitching moment equation; 8.4 Longitudinal manoeuvre stability; 8.5 Aircraft dynamics and manoeuvrability; References; Chapter 9. Stability; 9.1 Introduction; 9.2 The characteristic equation; 9.3 The Routh-Hurwitz stability criterion; 9.4 The stability quartic; 9.5 Graphical interpretation of stability; References; Problems; Chapter 10. Flying and handling qualities; 10.1 Introduction 327 $a10.2 Short term dynamic models10.3 Flying qualities requirements; 10.4 Aircraft role; 10.5 Pilot opinion rating; 10.6 Longitudinal flying qualities requirements; 10.7 Control anticipation parameter; 10.8 Lateral-directional flying qualities requirements; 10.9 Flying qualities requirements on the s-plane; References; Problems; Chapter 11. Stability augmentation; 11.1 Introduction; 11.2 Augmentation system design; 11.3 Closed loop system analysis; 11.4 The root locus plot; 11.5 Longitudinal stability augmentation; 11.6 Lateral-directional stability augmentation; 11.7 The pole placement method 327 $aReferences 330 $aThe study of flight dynamics requires a thorough understanding of the theory of the stability and control of aircraft, an appreciation of flight control systems and a comprehensive grounding in the theory of automatic control. Flight Dynamics provides all three in an accessible and student focussed text. Written for those coming to the subject for the first time the book is suitable as a complete first course text. It provides a secure foundation from which to move on to more advanced topics such a non-linear flight dynamics, simulation and advanced flight control, and is ideal for tho 410 0$aElsevier aerospace engineering series. 606 $aAerodynamics 606 $aFlight 606 $aStability of airplanes 615 0$aAerodynamics. 615 0$aFlight. 615 0$aStability of airplanes. 676 $a629.1 676 $a629.1323 700 $aCook$b M. V$01511563 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910784357203321 996 $aFlight dynamics principles$93744927 997 $aUNINA