| 000 | 02885nam a22004815i 4500 | ||
|---|---|---|---|
| 001 | 978-3-319-32238-4 | ||
| 003 | DE-He213 | ||
| 005 | 20200421112045.0 | ||
| 007 | cr nn 008mamaa | ||
| 008 | 160429s2016 gw | s |||| 0|eng d | ||
| 020 |
_a9783319322384 _9978-3-319-32238-4 |
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| 024 | 7 |
_a10.1007/978-3-319-32238-4 _2doi |
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| 050 | 4 | _aTJ212-225 | |
| 072 | 7 |
_aTJFM _2bicssc |
|
| 072 | 7 |
_aTEC004000 _2bisacsh |
|
| 082 | 0 | 4 |
_a629.8 _223 |
| 100 | 1 |
_aHamayun, Mirza Tariq. _eauthor. |
|
| 245 | 1 | 0 |
_aFault Tolerant Control Schemes Using Integral Sliding Modes _h[electronic resource] / _cby Mirza Tariq Hamayun, Christopher Edwards, Halim Alwi. |
| 264 | 1 |
_aCham : _bSpringer International Publishing : _bImprint: Springer, _c2016. |
|
| 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 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. | ||
| 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. |
|
| 700 | 1 |
_aAlwi, Halim. _eauthor. |
|
| 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 | _uhttp://dx.doi.org/10.1007/978-3-319-32238-4 |
| 912 | _aZDB-2-ENG | ||
| 942 | _cEBK | ||
| 999 |
_c56893 _d56893 |
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