Robust Surge Avoidance Control for a Low Pressure Compressor of a Turbojet Engine
Abstract The aim of this paper is to improve the efficiency of a low pressure compressor within a turbojet engine. For this purpose a new feedback controller will be introduced which compares the actual compressor surge margin to a given reference value. Then, this new feedback controller calculates...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Alt, Benedikt [verfasserIn] |
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| Format: |
Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2012 |
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| Schlagwörter: |
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| Anmerkung: |
© Springer Science+Business Media B.V. 2012 |
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| Übergeordnetes Werk: |
Enthalten in: Journal of intelligent & robotic systems - Springer Netherlands, 1988, 69(2012), 1-4 vom: 01. Aug., Seite 57-67 |
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| Übergeordnetes Werk: |
volume:69 ; year:2012 ; number:1-4 ; day:01 ; month:08 ; pages:57-67 |
| Links: |
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| DOI / URN: |
10.1007/s10846-012-9700-y |
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OLC2057176258 |
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| 520 | |a Abstract The aim of this paper is to improve the efficiency of a low pressure compressor within a turbojet engine. For this purpose a new feedback controller will be introduced which compares the actual compressor surge margin to a given reference value. Then, this new feedback controller calculates a deviation on the existing nozzle area schedule such that the overall efficiency of the controller is improved at steady state condition. The major contribution of this work consists in a robust control design approach leading to improved robustness properties and reduced calibration efforts for the controllers of future unmanned aircraft propulsion systems. | ||
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10.1007/s10846-012-9700-y doi (DE-627)OLC2057176258 (DE-He213)s10846-012-9700-y-p DE-627 ger DE-627 rakwb eng 004 VZ Alt, Benedikt verfasserin aut Robust Surge Avoidance Control for a Low Pressure Compressor of a Turbojet Engine 2012 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media B.V. 2012 Abstract The aim of this paper is to improve the efficiency of a low pressure compressor within a turbojet engine. For this purpose a new feedback controller will be introduced which compares the actual compressor surge margin to a given reference value. Then, this new feedback controller calculates a deviation on the existing nozzle area schedule such that the overall efficiency of the controller is improved at steady state condition. The major contribution of this work consists in a robust control design approach leading to improved robustness properties and reduced calibration efforts for the controllers of future unmanned aircraft propulsion systems. Energy efficient UAV systems Aircraft engine control Robust control Control applications Hermann, Elias aut Enthalten in Journal of intelligent & robotic systems Springer Netherlands, 1988 69(2012), 1-4 vom: 01. Aug., Seite 57-67 (DE-627)130464864 (DE-600)740594-7 (DE-576)018667805 0921-0296 nnns volume:69 year:2012 number:1-4 day:01 month:08 pages:57-67 https://doi.org/10.1007/s10846-012-9700-y lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-MAT GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2057 AR 69 2012 1-4 01 08 57-67 |
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10.1007/s10846-012-9700-y doi (DE-627)OLC2057176258 (DE-He213)s10846-012-9700-y-p DE-627 ger DE-627 rakwb eng 004 VZ Alt, Benedikt verfasserin aut Robust Surge Avoidance Control for a Low Pressure Compressor of a Turbojet Engine 2012 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media B.V. 2012 Abstract The aim of this paper is to improve the efficiency of a low pressure compressor within a turbojet engine. For this purpose a new feedback controller will be introduced which compares the actual compressor surge margin to a given reference value. Then, this new feedback controller calculates a deviation on the existing nozzle area schedule such that the overall efficiency of the controller is improved at steady state condition. The major contribution of this work consists in a robust control design approach leading to improved robustness properties and reduced calibration efforts for the controllers of future unmanned aircraft propulsion systems. Energy efficient UAV systems Aircraft engine control Robust control Control applications Hermann, Elias aut Enthalten in Journal of intelligent & robotic systems Springer Netherlands, 1988 69(2012), 1-4 vom: 01. Aug., Seite 57-67 (DE-627)130464864 (DE-600)740594-7 (DE-576)018667805 0921-0296 nnns volume:69 year:2012 number:1-4 day:01 month:08 pages:57-67 https://doi.org/10.1007/s10846-012-9700-y lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-MAT GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2057 AR 69 2012 1-4 01 08 57-67 |
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10.1007/s10846-012-9700-y doi (DE-627)OLC2057176258 (DE-He213)s10846-012-9700-y-p DE-627 ger DE-627 rakwb eng 004 VZ Alt, Benedikt verfasserin aut Robust Surge Avoidance Control for a Low Pressure Compressor of a Turbojet Engine 2012 Text txt rdacontent ohne Hilfsmittel zu benutzen n rdamedia Band nc rdacarrier © Springer Science+Business Media B.V. 2012 Abstract The aim of this paper is to improve the efficiency of a low pressure compressor within a turbojet engine. For this purpose a new feedback controller will be introduced which compares the actual compressor surge margin to a given reference value. Then, this new feedback controller calculates a deviation on the existing nozzle area schedule such that the overall efficiency of the controller is improved at steady state condition. The major contribution of this work consists in a robust control design approach leading to improved robustness properties and reduced calibration efforts for the controllers of future unmanned aircraft propulsion systems. Energy efficient UAV systems Aircraft engine control Robust control Control applications Hermann, Elias aut Enthalten in Journal of intelligent & robotic systems Springer Netherlands, 1988 69(2012), 1-4 vom: 01. Aug., Seite 57-67 (DE-627)130464864 (DE-600)740594-7 (DE-576)018667805 0921-0296 nnns volume:69 year:2012 number:1-4 day:01 month:08 pages:57-67 https://doi.org/10.1007/s10846-012-9700-y lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_OLC SSG-OLC-MAT GBV_ILN_70 GBV_ILN_2006 GBV_ILN_2057 AR 69 2012 1-4 01 08 57-67 |
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Abstract The aim of this paper is to improve the efficiency of a low pressure compressor within a turbojet engine. For this purpose a new feedback controller will be introduced which compares the actual compressor surge margin to a given reference value. Then, this new feedback controller calculates a deviation on the existing nozzle area schedule such that the overall efficiency of the controller is improved at steady state condition. The major contribution of this work consists in a robust control design approach leading to improved robustness properties and reduced calibration efforts for the controllers of future unmanned aircraft propulsion systems. © Springer Science+Business Media B.V. 2012 |
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Abstract The aim of this paper is to improve the efficiency of a low pressure compressor within a turbojet engine. For this purpose a new feedback controller will be introduced which compares the actual compressor surge margin to a given reference value. Then, this new feedback controller calculates a deviation on the existing nozzle area schedule such that the overall efficiency of the controller is improved at steady state condition. The major contribution of this work consists in a robust control design approach leading to improved robustness properties and reduced calibration efforts for the controllers of future unmanned aircraft propulsion systems. © Springer Science+Business Media B.V. 2012 |
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Abstract The aim of this paper is to improve the efficiency of a low pressure compressor within a turbojet engine. For this purpose a new feedback controller will be introduced which compares the actual compressor surge margin to a given reference value. Then, this new feedback controller calculates a deviation on the existing nozzle area schedule such that the overall efficiency of the controller is improved at steady state condition. The major contribution of this work consists in a robust control design approach leading to improved robustness properties and reduced calibration efforts for the controllers of future unmanned aircraft propulsion systems. © Springer Science+Business Media B.V. 2012 |
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<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">OLC2057176258</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230503115904.0</controlfield><controlfield tag="007">tu</controlfield><controlfield tag="008">200820s2012 xx ||||| 00| ||eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1007/s10846-012-9700-y</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)OLC2057176258</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-He213)s10846-012-9700-y-p</subfield></datafield><datafield tag="040" ind1=" " ind2=" "><subfield code="a">DE-627</subfield><subfield code="b">ger</subfield><subfield code="c">DE-627</subfield><subfield code="e">rakwb</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">004</subfield><subfield code="q">VZ</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Alt, Benedikt</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">Robust Surge Avoidance Control for a Low Pressure Compressor of a Turbojet Engine</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2012</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">Text</subfield><subfield code="b">txt</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">ohne Hilfsmittel zu benutzen</subfield><subfield code="b">n</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Band</subfield><subfield code="b">nc</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="500" ind1=" " ind2=" "><subfield code="a">© Springer Science+Business Media B.V. 2012</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Abstract The aim of this paper is to improve the efficiency of a low pressure compressor within a turbojet engine. For this purpose a new feedback controller will be introduced which compares the actual compressor surge margin to a given reference value. Then, this new feedback controller calculates a deviation on the existing nozzle area schedule such that the overall efficiency of the controller is improved at steady state condition. The major contribution of this work consists in a robust control design approach leading to improved robustness properties and reduced calibration efforts for the controllers of future unmanned aircraft propulsion systems.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Energy efficient UAV systems</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Aircraft engine control</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Robust control</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Control applications</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Hermann, Elias</subfield><subfield code="4">aut</subfield></datafield><datafield tag="773" ind1="0" ind2="8"><subfield code="i">Enthalten in</subfield><subfield code="t">Journal of intelligent & robotic systems</subfield><subfield code="d">Springer Netherlands, 1988</subfield><subfield code="g">69(2012), 1-4 vom: 01. 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