000 | 02927nam a22004815i 4500 | ||
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001 | 978-3-319-32238-4 | ||
003 | DE-He213 | ||
005 | 20180206182956.0 | ||
007 | cr nn 008mamaa | ||
008 | 160429s2016 gw | s |||| 0|eng d | ||
020 |
_a9783319322384 _9978-3-319-32238-4 |
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050 | 4 | _aTJ212-225 | |
072 | 7 |
_aTJFM _2bicssc |
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072 | 7 |
_aTEC004000 _2bisacsh |
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082 | 0 | 4 |
_a629.8 _223 |
100 | 1 |
_aHamayun, Mirza Tariq. _eauthor. |
|
245 | 1 | 0 |
_aFault Tolerant Control Schemes Using Integral Sliding Modes _h[recurso electrónico] / _cby Mirza Tariq Hamayun, Christopher Edwards, Halim Alwi. |
264 | 1 |
_aCham : _bSpringer International Publishing : _bImprint: Springer, _c2016. |
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300 |
_aXVIII, 199 p. 69 illus., 49 illus. in color. _bonline resource. |
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336 |
_atext _btxt _2rdacontent |
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337 |
_acomputer _bc _2rdamedia |
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338 |
_aonline resource _bcr _2rdacarrier |
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347 |
_atext file _bPDF _2rda |
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490 | 1 |
_aStudies in Systems, Decision and Control, _x2198-4182 ; _v61 |
|
520 | _aThe key attribute of a Fault Tolerant Control (FTC) system is its ability to maintainoverall system stability and acceptable performance in the face of faults andfailures within the feedback system. In this book Integral Sliding Mode (ISM) ControlAllocation (CA) schemes for FTC are described, which have the potential tomaintain close to nominal fault-free performance (for the entire system response),in the face of actuator faults and even complete failures of certain actuators. Broadlyan ISM controller based around a model of the plant with the aim of creating anonlinear fault tolerant feedback controller whose closed-loop performance is establishedduring the design process. The second approach involves retro-fitting anISM scheme to an existing feedback controller to introduce fault tolerance. Thismay be advantageous from an industrial perspective, because fault tolerance can beintroduced without changing the existing control loops. A high fidelity benchmarkmodel of a large transport aircraft is used to demonstrate the efficacy of the FTCschemes. In particular a scheme based on an LPV representation has been implementedand tested on a motion flight simulator. | ||
650 | 0 | _aEngineering. | |
650 | 0 | _aSystem theory. | |
650 | 0 | _aControl engineering. | |
650 | 1 | 4 | _aEngineering. |
650 | 2 | 4 | _aControl. |
650 | 2 | 4 | _aSystems Theory, Control. |
700 | 1 |
_aEdwards, Christopher. _eauthor. |
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700 | 1 |
_aAlwi, Halim. _eauthor. |
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710 | 2 | _aSpringerLink (Online service) | |
773 | 0 | _tSpringer eBooks | |
776 | 0 | 8 |
_iPrinted edition: _z9783319322360 |
830 | 0 |
_aStudies in Systems, Decision and Control, _x2198-4182 ; _v61 |
|
856 | 4 | 0 |
_zLibro electrónico _uhttp://148.231.10.114:2048/login?url=http://dx.doi.org/10.1007/978-3-319-32238-4 |
912 | _aZDB-2-ENG | ||
942 | _cLIBRO_ELEC | ||
999 |
_c225918 _d225918 |