Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft
Abstract To fill in the gap between theory and practice, this paper presents a gain-scheduled anti-windup proportional-integral-derivative (PID) control strategy for linear parameter-varying (LPV) systems with actuator saturation. Using the relationship between saturation and deadzone nonlinearities...
Ausführliche Beschreibung
Gespeichert in:
| Autor*in: |
Huang, Bixuan [verfasserIn] |
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| Format: |
E-Artikel |
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| Sprache: |
Englisch |
| Erschienen: |
2022 |
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| Schlagwörter: |
Linear parameter-varying systems |
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| Anmerkung: |
© Shanghai Jiao Tong University 2022 |
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| Übergeordnetes Werk: |
Enthalten in: Aerospace systems - Singapore : Springer Singapore, 2018, 5(2022), 3 vom: 12. Mai, Seite 445-454 |
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| Übergeordnetes Werk: |
volume:5 ; year:2022 ; number:3 ; day:12 ; month:05 ; pages:445-454 |
| Links: |
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| DOI / URN: |
10.1007/s42401-022-00143-z |
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| Katalog-ID: |
SPR047955228 |
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| 245 | 1 | 0 | |a Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft |
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| 520 | |a Abstract To fill in the gap between theory and practice, this paper presents a gain-scheduled anti-windup proportional-integral-derivative (PID) control strategy for linear parameter-varying (LPV) systems with actuator saturation. Using the relationship between saturation and deadzone nonlinearities, the resulting closed-loop system is recast into a system with a deadzone nonlinearity. With the aid of a parameter-dependent sector condition, the stability and %$\mathcal {L}_2%$ performance of the closed-loop system are elaborated using parameter-dependent Lyapunov approach. The developed synthesis condition is first formulated in terms of bilinear matrix inequalities (BMIs), which cannot be easily solved. Then, a set of linear matrix inequalities (LMIs) is derived by employing Finsler’s lemma. Finally, the proposed control strategy is applied to the flight control design of a lateral-directional aircraft system to illustrate its effectiveness and application potential. | ||
| 650 | 4 | |a Anti-windup control |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Linear parameter-varying systems |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Proportional-integral-derivative control |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Linear matrix inequalities |7 (dpeaa)DE-He213 | |
| 650 | 4 | |a Flight control |7 (dpeaa)DE-He213 | |
| 700 | 1 | |a Zhai, Mingyuan |4 aut | |
| 700 | 1 | |a Lu, Bei |0 (orcid)0000-0002-0351-5814 |4 aut | |
| 700 | 1 | |a Li, Qifu |4 aut | |
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10.1007/s42401-022-00143-z doi (DE-627)SPR047955228 (SPR)s42401-022-00143-z-e DE-627 ger DE-627 rakwb eng Huang, Bixuan verfasserin aut Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Shanghai Jiao Tong University 2022 Abstract To fill in the gap between theory and practice, this paper presents a gain-scheduled anti-windup proportional-integral-derivative (PID) control strategy for linear parameter-varying (LPV) systems with actuator saturation. Using the relationship between saturation and deadzone nonlinearities, the resulting closed-loop system is recast into a system with a deadzone nonlinearity. With the aid of a parameter-dependent sector condition, the stability and %$\mathcal {L}_2%$ performance of the closed-loop system are elaborated using parameter-dependent Lyapunov approach. The developed synthesis condition is first formulated in terms of bilinear matrix inequalities (BMIs), which cannot be easily solved. Then, a set of linear matrix inequalities (LMIs) is derived by employing Finsler’s lemma. Finally, the proposed control strategy is applied to the flight control design of a lateral-directional aircraft system to illustrate its effectiveness and application potential. Anti-windup control (dpeaa)DE-He213 Linear parameter-varying systems (dpeaa)DE-He213 Proportional-integral-derivative control (dpeaa)DE-He213 Linear matrix inequalities (dpeaa)DE-He213 Flight control (dpeaa)DE-He213 Zhai, Mingyuan aut Lu, Bei (orcid)0000-0002-0351-5814 aut Li, Qifu aut Enthalten in Aerospace systems Singapore : Springer Singapore, 2018 5(2022), 3 vom: 12. Mai, Seite 445-454 (DE-627)1035875527 (DE-600)2946651-9 2523-3955 nnns volume:5 year:2022 number:3 day:12 month:05 pages:445-454 https://dx.doi.org/10.1007/s42401-022-00143-z lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_266 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 5 2022 3 12 05 445-454 |
| spelling |
10.1007/s42401-022-00143-z doi (DE-627)SPR047955228 (SPR)s42401-022-00143-z-e DE-627 ger DE-627 rakwb eng Huang, Bixuan verfasserin aut Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Shanghai Jiao Tong University 2022 Abstract To fill in the gap between theory and practice, this paper presents a gain-scheduled anti-windup proportional-integral-derivative (PID) control strategy for linear parameter-varying (LPV) systems with actuator saturation. Using the relationship between saturation and deadzone nonlinearities, the resulting closed-loop system is recast into a system with a deadzone nonlinearity. With the aid of a parameter-dependent sector condition, the stability and %$\mathcal {L}_2%$ performance of the closed-loop system are elaborated using parameter-dependent Lyapunov approach. The developed synthesis condition is first formulated in terms of bilinear matrix inequalities (BMIs), which cannot be easily solved. Then, a set of linear matrix inequalities (LMIs) is derived by employing Finsler’s lemma. Finally, the proposed control strategy is applied to the flight control design of a lateral-directional aircraft system to illustrate its effectiveness and application potential. Anti-windup control (dpeaa)DE-He213 Linear parameter-varying systems (dpeaa)DE-He213 Proportional-integral-derivative control (dpeaa)DE-He213 Linear matrix inequalities (dpeaa)DE-He213 Flight control (dpeaa)DE-He213 Zhai, Mingyuan aut Lu, Bei (orcid)0000-0002-0351-5814 aut Li, Qifu aut Enthalten in Aerospace systems Singapore : Springer Singapore, 2018 5(2022), 3 vom: 12. Mai, Seite 445-454 (DE-627)1035875527 (DE-600)2946651-9 2523-3955 nnns volume:5 year:2022 number:3 day:12 month:05 pages:445-454 https://dx.doi.org/10.1007/s42401-022-00143-z lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_266 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 5 2022 3 12 05 445-454 |
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10.1007/s42401-022-00143-z doi (DE-627)SPR047955228 (SPR)s42401-022-00143-z-e DE-627 ger DE-627 rakwb eng Huang, Bixuan verfasserin aut Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Shanghai Jiao Tong University 2022 Abstract To fill in the gap between theory and practice, this paper presents a gain-scheduled anti-windup proportional-integral-derivative (PID) control strategy for linear parameter-varying (LPV) systems with actuator saturation. Using the relationship between saturation and deadzone nonlinearities, the resulting closed-loop system is recast into a system with a deadzone nonlinearity. With the aid of a parameter-dependent sector condition, the stability and %$\mathcal {L}_2%$ performance of the closed-loop system are elaborated using parameter-dependent Lyapunov approach. The developed synthesis condition is first formulated in terms of bilinear matrix inequalities (BMIs), which cannot be easily solved. Then, a set of linear matrix inequalities (LMIs) is derived by employing Finsler’s lemma. Finally, the proposed control strategy is applied to the flight control design of a lateral-directional aircraft system to illustrate its effectiveness and application potential. Anti-windup control (dpeaa)DE-He213 Linear parameter-varying systems (dpeaa)DE-He213 Proportional-integral-derivative control (dpeaa)DE-He213 Linear matrix inequalities (dpeaa)DE-He213 Flight control (dpeaa)DE-He213 Zhai, Mingyuan aut Lu, Bei (orcid)0000-0002-0351-5814 aut Li, Qifu aut Enthalten in Aerospace systems Singapore : Springer Singapore, 2018 5(2022), 3 vom: 12. Mai, Seite 445-454 (DE-627)1035875527 (DE-600)2946651-9 2523-3955 nnns volume:5 year:2022 number:3 day:12 month:05 pages:445-454 https://dx.doi.org/10.1007/s42401-022-00143-z lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_266 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 5 2022 3 12 05 445-454 |
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10.1007/s42401-022-00143-z doi (DE-627)SPR047955228 (SPR)s42401-022-00143-z-e DE-627 ger DE-627 rakwb eng Huang, Bixuan verfasserin aut Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Shanghai Jiao Tong University 2022 Abstract To fill in the gap between theory and practice, this paper presents a gain-scheduled anti-windup proportional-integral-derivative (PID) control strategy for linear parameter-varying (LPV) systems with actuator saturation. Using the relationship between saturation and deadzone nonlinearities, the resulting closed-loop system is recast into a system with a deadzone nonlinearity. With the aid of a parameter-dependent sector condition, the stability and %$\mathcal {L}_2%$ performance of the closed-loop system are elaborated using parameter-dependent Lyapunov approach. The developed synthesis condition is first formulated in terms of bilinear matrix inequalities (BMIs), which cannot be easily solved. Then, a set of linear matrix inequalities (LMIs) is derived by employing Finsler’s lemma. Finally, the proposed control strategy is applied to the flight control design of a lateral-directional aircraft system to illustrate its effectiveness and application potential. Anti-windup control (dpeaa)DE-He213 Linear parameter-varying systems (dpeaa)DE-He213 Proportional-integral-derivative control (dpeaa)DE-He213 Linear matrix inequalities (dpeaa)DE-He213 Flight control (dpeaa)DE-He213 Zhai, Mingyuan aut Lu, Bei (orcid)0000-0002-0351-5814 aut Li, Qifu aut Enthalten in Aerospace systems Singapore : Springer Singapore, 2018 5(2022), 3 vom: 12. Mai, Seite 445-454 (DE-627)1035875527 (DE-600)2946651-9 2523-3955 nnns volume:5 year:2022 number:3 day:12 month:05 pages:445-454 https://dx.doi.org/10.1007/s42401-022-00143-z lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_266 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 5 2022 3 12 05 445-454 |
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10.1007/s42401-022-00143-z doi (DE-627)SPR047955228 (SPR)s42401-022-00143-z-e DE-627 ger DE-627 rakwb eng Huang, Bixuan verfasserin aut Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft 2022 Text txt rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier © Shanghai Jiao Tong University 2022 Abstract To fill in the gap between theory and practice, this paper presents a gain-scheduled anti-windup proportional-integral-derivative (PID) control strategy for linear parameter-varying (LPV) systems with actuator saturation. Using the relationship between saturation and deadzone nonlinearities, the resulting closed-loop system is recast into a system with a deadzone nonlinearity. With the aid of a parameter-dependent sector condition, the stability and %$\mathcal {L}_2%$ performance of the closed-loop system are elaborated using parameter-dependent Lyapunov approach. The developed synthesis condition is first formulated in terms of bilinear matrix inequalities (BMIs), which cannot be easily solved. Then, a set of linear matrix inequalities (LMIs) is derived by employing Finsler’s lemma. Finally, the proposed control strategy is applied to the flight control design of a lateral-directional aircraft system to illustrate its effectiveness and application potential. Anti-windup control (dpeaa)DE-He213 Linear parameter-varying systems (dpeaa)DE-He213 Proportional-integral-derivative control (dpeaa)DE-He213 Linear matrix inequalities (dpeaa)DE-He213 Flight control (dpeaa)DE-He213 Zhai, Mingyuan aut Lu, Bei (orcid)0000-0002-0351-5814 aut Li, Qifu aut Enthalten in Aerospace systems Singapore : Springer Singapore, 2018 5(2022), 3 vom: 12. Mai, Seite 445-454 (DE-627)1035875527 (DE-600)2946651-9 2523-3955 nnns volume:5 year:2022 number:3 day:12 month:05 pages:445-454 https://dx.doi.org/10.1007/s42401-022-00143-z lizenzpflichtig Volltext GBV_USEFLAG_A SYSFLAG_A GBV_SPRINGER GBV_ILN_11 GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 GBV_ILN_39 GBV_ILN_40 GBV_ILN_60 GBV_ILN_62 GBV_ILN_63 GBV_ILN_65 GBV_ILN_69 GBV_ILN_70 GBV_ILN_73 GBV_ILN_74 GBV_ILN_90 GBV_ILN_95 GBV_ILN_100 GBV_ILN_105 GBV_ILN_110 GBV_ILN_138 GBV_ILN_150 GBV_ILN_151 GBV_ILN_152 GBV_ILN_161 GBV_ILN_170 GBV_ILN_171 GBV_ILN_187 GBV_ILN_213 GBV_ILN_224 GBV_ILN_230 GBV_ILN_250 GBV_ILN_266 GBV_ILN_281 GBV_ILN_285 GBV_ILN_293 GBV_ILN_370 GBV_ILN_602 GBV_ILN_636 GBV_ILN_702 GBV_ILN_2001 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2007 GBV_ILN_2008 GBV_ILN_2009 GBV_ILN_2010 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2026 GBV_ILN_2027 GBV_ILN_2031 GBV_ILN_2034 GBV_ILN_2037 GBV_ILN_2038 GBV_ILN_2039 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2055 GBV_ILN_2056 GBV_ILN_2057 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2093 GBV_ILN_2106 GBV_ILN_2107 GBV_ILN_2108 GBV_ILN_2110 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2144 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2188 GBV_ILN_2190 GBV_ILN_2232 GBV_ILN_2336 GBV_ILN_2446 GBV_ILN_2470 GBV_ILN_2472 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_2548 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4246 GBV_ILN_4249 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4306 GBV_ILN_4307 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4328 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4336 GBV_ILN_4338 GBV_ILN_4393 GBV_ILN_4700 AR 5 2022 3 12 05 445-454 |
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Enthalten in Aerospace systems 5(2022), 3 vom: 12. Mai, Seite 445-454 volume:5 year:2022 number:3 day:12 month:05 pages:445-454 |
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Huang, Bixuan @@aut@@ Zhai, Mingyuan @@aut@@ Lu, Bei @@aut@@ Li, Qifu @@aut@@ |
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Huang, Bixuan |
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Huang, Bixuan misc Anti-windup control misc Linear parameter-varying systems misc Proportional-integral-derivative control misc Linear matrix inequalities misc Flight control Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft |
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Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft Anti-windup control (dpeaa)DE-He213 Linear parameter-varying systems (dpeaa)DE-He213 Proportional-integral-derivative control (dpeaa)DE-He213 Linear matrix inequalities (dpeaa)DE-He213 Flight control (dpeaa)DE-He213 |
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misc Anti-windup control misc Linear parameter-varying systems misc Proportional-integral-derivative control misc Linear matrix inequalities misc Flight control |
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Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft |
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Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft |
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gain-scheduled anti-windup pid control for lpv systems under actuator saturation and its application to aircraft |
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Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft |
| abstract |
Abstract To fill in the gap between theory and practice, this paper presents a gain-scheduled anti-windup proportional-integral-derivative (PID) control strategy for linear parameter-varying (LPV) systems with actuator saturation. Using the relationship between saturation and deadzone nonlinearities, the resulting closed-loop system is recast into a system with a deadzone nonlinearity. With the aid of a parameter-dependent sector condition, the stability and %$\mathcal {L}_2%$ performance of the closed-loop system are elaborated using parameter-dependent Lyapunov approach. The developed synthesis condition is first formulated in terms of bilinear matrix inequalities (BMIs), which cannot be easily solved. Then, a set of linear matrix inequalities (LMIs) is derived by employing Finsler’s lemma. Finally, the proposed control strategy is applied to the flight control design of a lateral-directional aircraft system to illustrate its effectiveness and application potential. © Shanghai Jiao Tong University 2022 |
| abstractGer |
Abstract To fill in the gap between theory and practice, this paper presents a gain-scheduled anti-windup proportional-integral-derivative (PID) control strategy for linear parameter-varying (LPV) systems with actuator saturation. Using the relationship between saturation and deadzone nonlinearities, the resulting closed-loop system is recast into a system with a deadzone nonlinearity. With the aid of a parameter-dependent sector condition, the stability and %$\mathcal {L}_2%$ performance of the closed-loop system are elaborated using parameter-dependent Lyapunov approach. The developed synthesis condition is first formulated in terms of bilinear matrix inequalities (BMIs), which cannot be easily solved. Then, a set of linear matrix inequalities (LMIs) is derived by employing Finsler’s lemma. Finally, the proposed control strategy is applied to the flight control design of a lateral-directional aircraft system to illustrate its effectiveness and application potential. © Shanghai Jiao Tong University 2022 |
| abstract_unstemmed |
Abstract To fill in the gap between theory and practice, this paper presents a gain-scheduled anti-windup proportional-integral-derivative (PID) control strategy for linear parameter-varying (LPV) systems with actuator saturation. Using the relationship between saturation and deadzone nonlinearities, the resulting closed-loop system is recast into a system with a deadzone nonlinearity. With the aid of a parameter-dependent sector condition, the stability and %$\mathcal {L}_2%$ performance of the closed-loop system are elaborated using parameter-dependent Lyapunov approach. The developed synthesis condition is first formulated in terms of bilinear matrix inequalities (BMIs), which cannot be easily solved. Then, a set of linear matrix inequalities (LMIs) is derived by employing Finsler’s lemma. Finally, the proposed control strategy is applied to the flight control design of a lateral-directional aircraft system to illustrate its effectiveness and application potential. © Shanghai Jiao Tong University 2022 |
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Gain-scheduled anti-windup PID control for LPV systems under actuator saturation and its application to aircraft |
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https://dx.doi.org/10.1007/s42401-022-00143-z |
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Zhai, Mingyuan Lu, Bei Li, Qifu |
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Zhai, Mingyuan Lu, Bei Li, Qifu |
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| doi_str |
10.1007/s42401-022-00143-z |
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2024-07-03T16:06:05.214Z |
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