LEADER 03636nam 22005895 450 001 9910437769403321 005 20200701142544.0 010 $a3-642-36841-7 024 7 $a10.1007/978-3-642-36841-7 035 $a(CKB)2560000000105739 035 $a(SSID)ssj0000935374 035 $a(PQKBManifestationID)11518947 035 $a(PQKBTitleCode)TC0000935374 035 $a(PQKBWorkID)10954141 035 $a(PQKB)10319342 035 $a(DE-He213)978-3-642-36841-7 035 $a(MiAaPQ)EBC3096904 035 $a(PPN)170491161 035 $a(EXLCZ)992560000000105739 100 $a20130607d2013 u| 0 101 0 $aeng 135 $aurnn|008mamaa 181 $ctxt 182 $cc 183 $acr 200 10$aCompound Control Methodology for Flight Vehicles /$fby Yuanqing Xia, Mengyin Fu 205 $a1st ed. 2013. 210 1$aBerlin, Heidelberg :$cSpringer Berlin Heidelberg :$cImprint: Springer,$d2013. 215 $a1 online resource (XVIII, 260 p. 125 illus.) 225 1 $aLecture Notes in Control and Information Sciences,$x0170-8643 ;$v438 300 $aBibliographic Level Mode of Issuance: Monograph 311 $a3-642-36840-9 327 $aOverview of Sliding Mode Control -- Overview of Active Disturbance Rejection Control -- Overview of Flight Vehicle Control -- The Descriptions of Flight Vehicle -- SMC for Missile Systems Based on Back-Stepping and ESO Techniques -- Adaptive SMC for Attitude Stabilization in Presence of Actuator Saturation -- Adaptive Nonsingular Terminal Sliding Mode Control for Rigid Spacecraft -- Attitude Tracking of Rigid Spacecraft with Uncertainties and Disturbances -- SMC for Attitude Tracking of Rigid Spacecraft with Disturbances -- Missile Guidance Law Based on ESO Techniques -- Missile Guidance Laws Based on SMC and FTC Techniques -- Cooperative Attack of Multiple Missiles Based on Optimal Guidance Law. 330 $a?Compound Control Methodology for Flight Vehicles? focuses on new control methods for flight vehicles. In this monograph the concept of compound control is introduced. It is demonstrated that both Sliding Mode Control (SMC) and Active Disturbance Rejection Control (ADRC) have their own advantages and limitations, i.e., chattering of SMC and the observability of extended state observer (ESO), respectively. It is shown that compound control combines their advantages and improves the performance of the closed-loop systems. The book is self-contained, providing sufficient mathematical foundations for understanding the contents of each chapter. It will be of significant interest to scientists and engineers engaged in the field of flight vehicle control. 410 0$aLecture Notes in Control and Information Sciences,$x0170-8643 ;$v438 606 $aControl engineering 606 $aAerospace engineering 606 $aAstronautics 606 $aControl and Systems Theory$3https://scigraph.springernature.com/ontologies/product-market-codes/T19010 606 $aAerospace Technology and Astronautics$3https://scigraph.springernature.com/ontologies/product-market-codes/T17050 615 0$aControl engineering. 615 0$aAerospace engineering. 615 0$aAstronautics. 615 14$aControl and Systems Theory. 615 24$aAerospace Technology and Astronautics. 676 $a629.8 700 $aXia$b Yuanqing$4aut$4http://id.loc.gov/vocabulary/relators/aut$0739922 702 $aFu$b Mengyin$4aut$4http://id.loc.gov/vocabulary/relators/aut 906 $aBOOK 912 $a9910437769403321 996 $aCompound Control Methodology for Flight Vehicles$92497914 997 $aUNINA