Fault Tolerant Control Schemes Using Integral Sliding Modes (Record no. 56893)
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000 -LEADER | |
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fixed length control field | 02885nam a22004815i 4500 |
001 - CONTROL NUMBER | |
control field | 978-3-319-32238-4 |
005 - DATE AND TIME OF LATEST TRANSACTION | |
control field | 20200421112045.0 |
008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
fixed length control field | 160429s2016 gw | s |||| 0|eng d |
020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
ISBN | 9783319322384 |
-- | 978-3-319-32238-4 |
082 04 - CLASSIFICATION NUMBER | |
Call Number | 629.8 |
100 1# - AUTHOR NAME | |
Author | Hamayun, Mirza Tariq. |
245 10 - TITLE STATEMENT | |
Title | Fault Tolerant Control Schemes Using Integral Sliding Modes |
300 ## - PHYSICAL DESCRIPTION | |
Number of Pages | XVIII, 199 p. 69 illus., 49 illus. in color. |
490 1# - SERIES STATEMENT | |
Series statement | Studies in Systems, Decision and Control, |
520 ## - SUMMARY, ETC. | |
Summary, etc | The 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. |
700 1# - AUTHOR 2 | |
Author 2 | Edwards, Christopher. |
700 1# - AUTHOR 2 | |
Author 2 | Alwi, Halim. |
856 40 - ELECTRONIC LOCATION AND ACCESS | |
Uniform Resource Identifier | http://dx.doi.org/10.1007/978-3-319-32238-4 |
942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
Koha item type | eBooks |
264 #1 - | |
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-- | Springer International Publishing : |
-- | Imprint: Springer, |
-- | 2016. |
336 ## - | |
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-- | txt |
-- | rdacontent |
337 ## - | |
-- | computer |
-- | c |
-- | rdamedia |
338 ## - | |
-- | online resource |
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347 ## - | |
-- | text file |
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650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Engineering. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | System theory. |
650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Control engineering. |
650 14 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Engineering. |
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Control. |
650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
-- | Systems Theory, Control. |
830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE | |
-- | 2198-4182 ; |
912 ## - | |
-- | ZDB-2-ENG |
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