000			03597nam a22004095i 4500
001			85901
003			ES-MaUEC
005			20230207040533.0
007			cr nn 008mamaa
008			160429s2016 gw | s |||| 0|eng d
020			_a9783319322384
040			_aES-MaUEC
050		4	_aTJ220.5 _bH363 2016
082	0	4	_a629.8
100	1		_aHamayun, Mirza Tariq _0Local _999203
245	1	0	_aFault Tolerant Control Schemes Using Integral Sliding Modes _cby Mirza Tariq Hamayun, Christopher Edwards, Halim Alwi
260			_aCham _bSpringer International Publishing _c2016
300			_a1 recurso en línea (XVIII, 199 páginas) _b69 ilustraciones, 49 ilustraciones en color
336			_aTexto _btxt _2rdacontent
337			_aelectrónico _bc _2rdamedia
338			_arecurso electrónico _bcr _2rdacarrier
490	0		_aStudies in Systems, Decision and Control _x2198-4182 _v61
505	0		_aFault Tolerant Control -- Integral Sliding Mode Control -- Design and Analysis of an Integral Sliding Mode Fault Tolerant Control Scheme -- A Fault Tolerant Direct Control Allocation Scheme with Integral Sliding Modes -- An Output Integral Sliding Mode FTC Scheme Using Control Allocation -- An Augmentation Scheme for Fault Tolerant Control using Integral Sliding Modes -- Nonlinear Integral Sliding Mode -- Linear Parameter Varying FTC Scheme Using Integral Sliding Modes -- Real-Time Implementation of an ISM Fault Tolerant Control Scheme on the SIMONA Flight Simulator -- Benchmark Model of Large Transport Aircraft -- Closed-Loop Stability and Feedback Gain Synthesis.
520	3		_aThe key attribute of a Fault Tolerant Control (FTC) system is its ability to maintain overall system stability and acceptable performance in the face of faults and failures within the feedback system. In this book Integral Sliding Mode (ISM) Control Allocation (CA) schemes for FTC are described, which have the potential to maintain close to nominal fault-free performance (for the entire system response), in the face of actuator faults and even complete failures of certain actuators. Broadly an ISM controller based around a model of the plant with the aim of creating a nonlinear fault tolerant feedback controller whose closed-loop performance is established during the design process. The second approach involves retro-fitting an ISM scheme to an existing feedback controller to introduce fault tolerance. This may be advantageous from an industrial perspective, because fault tolerance can be introduced without changing the existing control loops. A high fidelity benchmark model of a large transport aircraft is used to demonstrate the efficacy of the FTC schemes. In particular a scheme based on an LPV representation has been implemented and tested on a motion flight simulator.
710	2		_aSpringerLink (Online service) _0Local _9106996
942			_2lcc _cLE
988			_aEBOOK, asignarmaterias , EBSPRINGER
650	0	7	_aSistemas, Teoría de _0 _2embne _9141328
650	0	7	_aControl automático _0 _2embne _9405125
700	1		_aEdwards, Christopher. _96390 _0comprobar BNE19940393870
700	1		_aAlwi, Halim _0Local _999204
856	4	0	_uhttps://go.openathens.net/redirector/universidadeuropea.es?url=https://link.springer.com/book/10.1007/978-3-319-32238-4 _zAcceso a este recurso digital (usuarios Universidad Europea de Madrid)
901			_ai9783319322384
907			_a.b12951791 _b10-10-17 _c21-11-16
998			_am _a_alco _a_vill _b - - _cm _dz _e- _feng _ggw _h0
945			_aTJ220.5 H363 2016 EB _g1 _ieBOOK _j0 _lmae _o- _pEUR0.00 _q- _r- _sb _t15 _u0 _v0 _w0 _x0 _y.i11594561 _z06-04-17
999			_c85901 _d85901 _x1