LEADER 03448nam 2200565 a 450 001 9910796091203321 005 20200520144314.0 010 0 $a9781118646793 010 0 $a1118646797 035 $a(MiAaPQ)EBC7103912 035 $a(CKB)24989724600041 035 $a(MiAaPQ)EBC1319130 035 $a(Au-PeEL)EBL1319130 035 $a(CaPaEBR)ebr10735223 035 $a(CaONFJC)MIL527854 035 $a(OCoLC)854521096 035 $a(NjHacI)9924989724600041 035 $a(JP-MeL)3000111584 035 $a(Au-PeEL)EBL7103912 035 $a(OCoLC)1347023353 035 $a(EXLCZ)9924989724600041 100 $a20130515d2013 uy 0 101 0 $aeng 135 $aur||||||||||| 181 $ctxt$2rdacontent 182 $cc$2rdamedia 183 $acr$2rdacarrier 200 10$aAircraft flight dynamics and control$b[electronic resource] /$fWayne Durham 210 $aChichester, West Sussex $cJohn Wiley & Sons, Inc.$d2013 215 $axix, 286 p. $cill 225 1 $aAerospace series 320 $aIncludes bibliographical references and index. 330 $aAircraft Flight Dynamics and Control addresses airplane flight dynamics and control in a largely classical manner, but with references to modern treatment throughout. Classical feedback control methods are illustrated with relevant examples, and current trends in control are presented by introductions to dynamic inversion and control allocation. This book covers the physical and mathematical fundamentals of aircraft flight dynamics as well as more advanced theory enabling a better insight into nonlinear dynamics. This leads to a useful introduction to automatic flight control and stability augmentation systems with discussion of the theory behind their design, and the limitations of the systems. The author provides a rigorous development of theory and derivations and illustrates the equations of motion in both scalar and matrix notation. Key features: Classical development and modern treatment of flight dynamics and control Detailed and rigorous exposition and examples, with illustrations Presentation of important trends in modern flight control systems Accessible introduction to control allocation based on the author's seminal work in the field Development of sensitivity analysis to determine the influential states in an airplane's response modes End of chapter problems with solutions available on an accompanying website Written by an author with experience as an engineering test pilot as well as a university professor, Aircraft Flight Dynamics and Control provides the reader with a systematic development of the insights and tools necessary for further work in related fields of flight dynamics and control. It is an ideal course textbook and is also a valuable reference for many of the necessary basic formulations of the math and science underlying flight dynamics and control. 410 0$aAerospace series (Chichester, England) 606 $aAerodynamics 606 $aAirplanes$xPerformance 606 $aFlight control 606 $aFlight 615 0$aAerodynamics. 615 0$aAirplanes$xPerformance. 615 0$aFlight control. 615 0$aFlight. 676 $a629.132/3 700 $aDurham$b Wayne$f1941-$0900575 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 912 $a9910796091203321 996 $aAircraft flight dynamics and control$93754785 997 $aUNINA