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020 _a9783642368417
_99783642368417
024 7 _a10.1007/9783642368417
_2doi
035 _avtls000361137
039 9 _a201509030619
_bVLOAD
_c201405070310
_dVLOAD
_y201402210941
_zstaff
040 _aMX-SnUAN
_bspa
_cMX-SnUAN
_erda
050 4 _aTJ212-225
100 1 _9445940
_aXia, Yuanqing
_eautor
245 1 0 _aCompound Control Methodology for Flight Vehicles /
_cby Yuanqing Xia, Mengyin Fu.
264 1 _aBerlin, Heidelberg :
_bSpringer Berlin Heidelberg :
_bImprint: Springer,
_c2013.
300 _axviii, 260 páginas 125 ilustraciones
_brecurso en línea.
336 _atexto
_btxt
_2rdacontent
337 _acomputadora
_bc
_2rdamedia
338 _arecurso en línea
_bcr
_2rdacarrier
347 _aarchivo de texto
_bPDF
_2rda
490 0 _aLecture Notes in Control and Information Sciences,
_x0170-8643 ;
_v438
500 _aSpringer eBooks
505 0 _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.
520 _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.
590 _aPara consulta fuera de la UANL se requiere clave de acceso remoto.
700 1 _aFu, Mengyin.
_eautor
_9338119
710 2 _aSpringerLink (Servicio en línea)
_9299170
776 0 8 _iEdición impresa:
_z9783642368400
856 4 0 _uhttp://remoto.dgb.uanl.mx/login?url=http://dx.doi.org/10.1007/978-3-642-36841-7
_zConectar a Springer E-Books (Para consulta externa se requiere previa autentificación en Biblioteca Digital UANL)
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999 _c306970
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