LEADER 03924nam 2200613 a 450 001 9910967130803321 005 20240416073039.0 010 $a1-60086-734-0 010 $a1-60086-733-2 010 $a1-61344-043-X 035 $a(CKB)3390000000018385 035 $a(SSID)ssj0000550789 035 $a(PQKBManifestationID)12204456 035 $a(PQKBTitleCode)TC0000550789 035 $a(PQKBWorkID)10524225 035 $a(PQKB)11148529 035 $a(MiAaPQ)EBC3111516 035 $a(Au-PeEL)EBL3111516 035 $a(CaPaEBR)ebr10516620 035 $a(OCoLC)922978930 035 $a(BIP)28295142 035 $a(EXLCZ)993390000000018385 100 $a20091022d2010 uy 0 101 0 $aeng 135 $aurcn||||||||| 181 $ctxt 182 $cc 183 $acr 200 10$aOptimal control theory with aerospace applications /$fJoseph Z. Ben-Asher 205 $a1st ed. 210 $aReston, Va. $cAmerican Institute of Aeronautics and Astronautics, Inc.$dc2010 215 $axvii, 262 p. $cill 225 1 $aAIAA education series 300 $aBibliographic Level Mode of Issuance: Monograph 311 08$a1-60086-732-4 320 $aIncludes bibliographical references and index. 327 $aHistorical background -- Ordinary minimum problems : from the beginning of calculus to Kuhn-Tucker -- Calculus of variations : from Bernoulli to Bliss -- Minimum principle of Pontryagin and Hestenes -- Application of the Jacobi test in optimal control and neighboring extremals -- Numerical techniques for the optimal control problem -- Singular perturbation technique and its application to air-to-space interception -- Application to aircraft performance : Rutowski and Kaiser's techniques and more -- Application to rocket performance : the Goddard problem -- Application to missile guidance : proportional navigation -- Application to time-optimal rotational maneuvers of flexible spacecraft. 330 $aOptimal control theory is a mathematical optimization method with important applications in the aerospace industry. This graduate-level textbook is based on the author's two decades of teaching at Tel-Aviv University and the Technion Israel Institute of Technology, and builds upon the pioneering methodologies developed by H.J. Kelley. Unlike other books on the subject, the text places optimal control theory within a historical perspective. Following the historical introduction are five chapters dealing with theory and five dealing with primarily aerospace applications. The theoretical section follows the calculus of variations approach, while also covering topics such as gradient methods, adjoint analysis, hodograph perspectives, and singular control. Important examples such as Zermelo's navigation problem are addressed throughout the theoretical chapters of the book. The applications section contains case studies in areas such as atmospheric flight, rocket performance, and missile guidance. The cases chosen are those that demonstrate some new computational aspects, are historically important, or are connected to the legacy of H.J. Kelley.To keep the mathematical level at that of graduate students in engineering, rigorous proofs of many important results are not given, while the interested reader is referred to more mathematical sources. Problem sets are also included. 410 0$aAIAA education series. 606 $aAutomatic pilot (Airplanes) 606 $aFlight control 606 $aGuided missiles$xControl systems 615 0$aAutomatic pilot (Airplanes) 615 0$aFlight control. 615 0$aGuided missiles$xControl systems. 676 $a629.132/6 700 $aBen-Asher$b Joseph Z.$f1955-$01872357 801 0$bMiAaPQ 801 1$bMiAaPQ 801 2$bMiAaPQ 906 $aBOOK 912 $a9910967130803321 996 $aOptimal control theory with aerospace applications$94481491 997 $aUNINA