The lateral control during aircraft-on-ground deceleration phases

Lateral control during aircraft-on-ground deceleration, which is one of the most important issues in aircraft-on-ground maneuvers, is discussed in this paper. Based on linear quadratic and predictive control theories, two controllers are developed to replace pilot control, which is effective only to...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Dai, Yaqi [verfasserIn] Song, Jian [verfasserIn] Yu, Liangyao [verfasserIn] Lu, Zhenghong [verfasserIn] Zheng, Sheng [verfasserIn] Li, Fei [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2019

Schlagwörter:	Aircraft-on-ground Lateral dynamics control Parameter variation Nonlinear system Linear quadratic control Predictive control

Übergeordnetes Werk:	Enthalten in: Aerospace science and technology - Amsterdam [u.a.] : Elsevier Science, 1997, 95
Übergeordnetes Werk:	volume:95

DOI / URN:	10.1016/j.ast.2019.105482

Katalog-ID:	ELV003257924

Internformat


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245	1	0	\|a The lateral control during aircraft-on-ground deceleration phases
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520			\|a Lateral control during aircraft-on-ground deceleration, which is one of the most important issues in aircraft-on-ground maneuvers, is discussed in this paper. Based on linear quadratic and predictive control theories, two controllers are developed to replace pilot control, which is effective only to a limited level under severe conditions. Particularly, because the aircraft forward speed decreases during deceleration, we propose a novel weighted model predictive control (MPC) method to control this parameter-varying system. Under the same severe conditions, simulation results show different efficiencies for these two controllers and both exhibited better performance than pilot control.
650		4	\|a Aircraft-on-ground
650		4	\|a Lateral dynamics control
650		4	\|a Parameter variation
650		4	\|a Nonlinear system
650		4	\|a Linear quadratic control
650		4	\|a Predictive control
700	1		\|a Song, Jian \|e verfasserin \|4 aut
700	1		\|a Yu, Liangyao \|e verfasserin \|4 aut
700	1		\|a Lu, Zhenghong \|e verfasserin \|4 aut
700	1		\|a Zheng, Sheng \|e verfasserin \|4 aut
700	1		\|a Li, Fei \|e verfasserin \|4 aut
773	0	8	\|i Enthalten in \|t Aerospace science and technology \|d Amsterdam [u.a.] : Elsevier Science, 1997 \|g 95 \|h Online-Ressource \|w (DE-627)320521486 \|w (DE-600)2014638-3 \|w (DE-576)255630425 \|x 1626-3219 \|7 nnns
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author_variant	y d yd j s js l y ly z l zl s z sz f l fl
matchkey_str	article:16263219:2019----::hltrlotodrnarrfogondc
hierarchy_sort_str	2019
bklnumber	55.50 55.60
publishDate	2019
allfields	10.1016/j.ast.2019.105482 doi (DE-627)ELV003257924 (ELSEVIER)S1270-9638(18)31363-4 DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Dai, Yaqi verfasserin aut The lateral control during aircraft-on-ground deceleration phases 2019 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Lateral control during aircraft-on-ground deceleration, which is one of the most important issues in aircraft-on-ground maneuvers, is discussed in this paper. Based on linear quadratic and predictive control theories, two controllers are developed to replace pilot control, which is effective only to a limited level under severe conditions. Particularly, because the aircraft forward speed decreases during deceleration, we propose a novel weighted model predictive control (MPC) method to control this parameter-varying system. Under the same severe conditions, simulation results show different efficiencies for these two controllers and both exhibited better performance than pilot control. Aircraft-on-ground Lateral dynamics control Parameter variation Nonlinear system Linear quadratic control Predictive control Song, Jian verfasserin aut Yu, Liangyao verfasserin aut Lu, Zhenghong verfasserin aut Zheng, Sheng verfasserin aut Li, Fei verfasserin aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 95 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:95 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 55.50 Luftfahrzeugtechnik 55.60 Raumfahrttechnik 55.60 Raumfahrttechnik AR 95
spelling	10.1016/j.ast.2019.105482 doi (DE-627)ELV003257924 (ELSEVIER)S1270-9638(18)31363-4 DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Dai, Yaqi verfasserin aut The lateral control during aircraft-on-ground deceleration phases 2019 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Lateral control during aircraft-on-ground deceleration, which is one of the most important issues in aircraft-on-ground maneuvers, is discussed in this paper. Based on linear quadratic and predictive control theories, two controllers are developed to replace pilot control, which is effective only to a limited level under severe conditions. Particularly, because the aircraft forward speed decreases during deceleration, we propose a novel weighted model predictive control (MPC) method to control this parameter-varying system. Under the same severe conditions, simulation results show different efficiencies for these two controllers and both exhibited better performance than pilot control. Aircraft-on-ground Lateral dynamics control Parameter variation Nonlinear system Linear quadratic control Predictive control Song, Jian verfasserin aut Yu, Liangyao verfasserin aut Lu, Zhenghong verfasserin aut Zheng, Sheng verfasserin aut Li, Fei verfasserin aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 95 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:95 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 55.50 Luftfahrzeugtechnik 55.60 Raumfahrttechnik 55.60 Raumfahrttechnik AR 95
allfields_unstemmed	10.1016/j.ast.2019.105482 doi (DE-627)ELV003257924 (ELSEVIER)S1270-9638(18)31363-4 DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Dai, Yaqi verfasserin aut The lateral control during aircraft-on-ground deceleration phases 2019 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Lateral control during aircraft-on-ground deceleration, which is one of the most important issues in aircraft-on-ground maneuvers, is discussed in this paper. Based on linear quadratic and predictive control theories, two controllers are developed to replace pilot control, which is effective only to a limited level under severe conditions. Particularly, because the aircraft forward speed decreases during deceleration, we propose a novel weighted model predictive control (MPC) method to control this parameter-varying system. Under the same severe conditions, simulation results show different efficiencies for these two controllers and both exhibited better performance than pilot control. Aircraft-on-ground Lateral dynamics control Parameter variation Nonlinear system Linear quadratic control Predictive control Song, Jian verfasserin aut Yu, Liangyao verfasserin aut Lu, Zhenghong verfasserin aut Zheng, Sheng verfasserin aut Li, Fei verfasserin aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 95 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:95 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 55.50 Luftfahrzeugtechnik 55.60 Raumfahrttechnik 55.60 Raumfahrttechnik AR 95
allfieldsGer	10.1016/j.ast.2019.105482 doi (DE-627)ELV003257924 (ELSEVIER)S1270-9638(18)31363-4 DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Dai, Yaqi verfasserin aut The lateral control during aircraft-on-ground deceleration phases 2019 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Lateral control during aircraft-on-ground deceleration, which is one of the most important issues in aircraft-on-ground maneuvers, is discussed in this paper. Based on linear quadratic and predictive control theories, two controllers are developed to replace pilot control, which is effective only to a limited level under severe conditions. Particularly, because the aircraft forward speed decreases during deceleration, we propose a novel weighted model predictive control (MPC) method to control this parameter-varying system. Under the same severe conditions, simulation results show different efficiencies for these two controllers and both exhibited better performance than pilot control. Aircraft-on-ground Lateral dynamics control Parameter variation Nonlinear system Linear quadratic control Predictive control Song, Jian verfasserin aut Yu, Liangyao verfasserin aut Lu, Zhenghong verfasserin aut Zheng, Sheng verfasserin aut Li, Fei verfasserin aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 95 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:95 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 55.50 Luftfahrzeugtechnik 55.60 Raumfahrttechnik 55.60 Raumfahrttechnik AR 95
allfieldsSound	10.1016/j.ast.2019.105482 doi (DE-627)ELV003257924 (ELSEVIER)S1270-9638(18)31363-4 DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Dai, Yaqi verfasserin aut The lateral control during aircraft-on-ground deceleration phases 2019 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier Lateral control during aircraft-on-ground deceleration, which is one of the most important issues in aircraft-on-ground maneuvers, is discussed in this paper. Based on linear quadratic and predictive control theories, two controllers are developed to replace pilot control, which is effective only to a limited level under severe conditions. Particularly, because the aircraft forward speed decreases during deceleration, we propose a novel weighted model predictive control (MPC) method to control this parameter-varying system. Under the same severe conditions, simulation results show different efficiencies for these two controllers and both exhibited better performance than pilot control. Aircraft-on-ground Lateral dynamics control Parameter variation Nonlinear system Linear quadratic control Predictive control Song, Jian verfasserin aut Yu, Liangyao verfasserin aut Lu, Zhenghong verfasserin aut Zheng, Sheng verfasserin aut Li, Fei verfasserin aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 95 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:95 GBV_USEFLAG_U SYSFLAG_U GBV_ELV SSG-OPC-AST GBV_ILN_20 GBV_ILN_22 GBV_ILN_23 GBV_ILN_24 GBV_ILN_31 GBV_ILN_32 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_150 GBV_ILN_151 GBV_ILN_224 GBV_ILN_370 GBV_ILN_602 GBV_ILN_702 GBV_ILN_2003 GBV_ILN_2004 GBV_ILN_2005 GBV_ILN_2006 GBV_ILN_2008 GBV_ILN_2011 GBV_ILN_2014 GBV_ILN_2015 GBV_ILN_2020 GBV_ILN_2021 GBV_ILN_2025 GBV_ILN_2027 GBV_ILN_2034 GBV_ILN_2038 GBV_ILN_2044 GBV_ILN_2048 GBV_ILN_2049 GBV_ILN_2050 GBV_ILN_2056 GBV_ILN_2059 GBV_ILN_2061 GBV_ILN_2064 GBV_ILN_2065 GBV_ILN_2068 GBV_ILN_2088 GBV_ILN_2111 GBV_ILN_2112 GBV_ILN_2113 GBV_ILN_2118 GBV_ILN_2122 GBV_ILN_2129 GBV_ILN_2143 GBV_ILN_2147 GBV_ILN_2148 GBV_ILN_2152 GBV_ILN_2153 GBV_ILN_2190 GBV_ILN_2336 GBV_ILN_2470 GBV_ILN_2507 GBV_ILN_2522 GBV_ILN_4035 GBV_ILN_4037 GBV_ILN_4046 GBV_ILN_4112 GBV_ILN_4125 GBV_ILN_4126 GBV_ILN_4242 GBV_ILN_4251 GBV_ILN_4305 GBV_ILN_4313 GBV_ILN_4322 GBV_ILN_4323 GBV_ILN_4324 GBV_ILN_4325 GBV_ILN_4326 GBV_ILN_4333 GBV_ILN_4334 GBV_ILN_4335 GBV_ILN_4338 GBV_ILN_4393 55.50 Luftfahrzeugtechnik 55.60 Raumfahrttechnik 55.60 Raumfahrttechnik AR 95
language	English
source	Enthalten in Aerospace science and technology 95 volume:95
sourceStr	Enthalten in Aerospace science and technology 95 volume:95
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bklname	Luftfahrzeugtechnik Raumfahrttechnik
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topic_facet	Aircraft-on-ground Lateral dynamics control Parameter variation Nonlinear system Linear quadratic control Predictive control
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authorswithroles_txt_mv	Dai, Yaqi @@aut@@ Song, Jian @@aut@@ Yu, Liangyao @@aut@@ Lu, Zhenghong @@aut@@ Zheng, Sheng @@aut@@ Li, Fei @@aut@@
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author	Dai, Yaqi
spellingShingle	Dai, Yaqi ddc 620 bkl 55.50 bkl 55.60 misc Aircraft-on-ground misc Lateral dynamics control misc Parameter variation misc Nonlinear system misc Linear quadratic control misc Predictive control The lateral control during aircraft-on-ground deceleration phases
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topic_title	620 DE-600 55.50 bkl 55.60 bkl The lateral control during aircraft-on-ground deceleration phases Aircraft-on-ground Lateral dynamics control Parameter variation Nonlinear system Linear quadratic control Predictive control
topic	ddc 620 bkl 55.50 bkl 55.60 misc Aircraft-on-ground misc Lateral dynamics control misc Parameter variation misc Nonlinear system misc Linear quadratic control misc Predictive control
topic_unstemmed	ddc 620 bkl 55.50 bkl 55.60 misc Aircraft-on-ground misc Lateral dynamics control misc Parameter variation misc Nonlinear system misc Linear quadratic control misc Predictive control
topic_browse	ddc 620 bkl 55.50 bkl 55.60 misc Aircraft-on-ground misc Lateral dynamics control misc Parameter variation misc Nonlinear system misc Linear quadratic control misc Predictive control
format_facet	Elektronische Aufsätze Aufsätze Elektronische Ressource
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title	The lateral control during aircraft-on-ground deceleration phases
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title_full	The lateral control during aircraft-on-ground deceleration phases
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title_sort	the lateral control during aircraft-on-ground deceleration phases
title_auth	The lateral control during aircraft-on-ground deceleration phases
abstract	Lateral control during aircraft-on-ground deceleration, which is one of the most important issues in aircraft-on-ground maneuvers, is discussed in this paper. Based on linear quadratic and predictive control theories, two controllers are developed to replace pilot control, which is effective only to a limited level under severe conditions. Particularly, because the aircraft forward speed decreases during deceleration, we propose a novel weighted model predictive control (MPC) method to control this parameter-varying system. Under the same severe conditions, simulation results show different efficiencies for these two controllers and both exhibited better performance than pilot control.
abstractGer	Lateral control during aircraft-on-ground deceleration, which is one of the most important issues in aircraft-on-ground maneuvers, is discussed in this paper. Based on linear quadratic and predictive control theories, two controllers are developed to replace pilot control, which is effective only to a limited level under severe conditions. Particularly, because the aircraft forward speed decreases during deceleration, we propose a novel weighted model predictive control (MPC) method to control this parameter-varying system. Under the same severe conditions, simulation results show different efficiencies for these two controllers and both exhibited better performance than pilot control.
abstract_unstemmed	Lateral control during aircraft-on-ground deceleration, which is one of the most important issues in aircraft-on-ground maneuvers, is discussed in this paper. Based on linear quadratic and predictive control theories, two controllers are developed to replace pilot control, which is effective only to a limited level under severe conditions. Particularly, because the aircraft forward speed decreases during deceleration, we propose a novel weighted model predictive control (MPC) method to control this parameter-varying system. Under the same severe conditions, simulation results show different efficiencies for these two controllers and both exhibited better performance than pilot control.
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title_short	The lateral control during aircraft-on-ground deceleration phases
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up_date	2024-07-06T19:01:27.004Z
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fullrecord_marcxml	<?xml version="1.0" encoding="UTF-8"?><collection xmlns="http://www.loc.gov/MARC21/slim"><record><leader>01000caa a22002652 4500</leader><controlfield tag="001">ELV003257924</controlfield><controlfield tag="003">DE-627</controlfield><controlfield tag="005">20230524151607.0</controlfield><controlfield tag="007">cr uuu---uuuuu</controlfield><controlfield tag="008">230430s2019 xx \|\|\|\|\|o 00\| \|\|eng c</controlfield><datafield tag="024" ind1="7" ind2=" "><subfield code="a">10.1016/j.ast.2019.105482</subfield><subfield code="2">doi</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(DE-627)ELV003257924</subfield></datafield><datafield tag="035" ind1=" " ind2=" "><subfield code="a">(ELSEVIER)S1270-9638(18)31363-4</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">rda</subfield></datafield><datafield tag="041" ind1=" " ind2=" "><subfield code="a">eng</subfield></datafield><datafield tag="082" ind1="0" ind2="4"><subfield code="a">620</subfield><subfield code="q">DE-600</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">55.50</subfield><subfield code="2">bkl</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">55.60</subfield><subfield code="2">bkl</subfield></datafield><datafield tag="084" ind1=" " ind2=" "><subfield code="a">55.60</subfield><subfield code="2">bkl</subfield></datafield><datafield tag="100" ind1="1" ind2=" "><subfield code="a">Dai, Yaqi</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="245" ind1="1" ind2="0"><subfield code="a">The lateral control during aircraft-on-ground deceleration phases</subfield></datafield><datafield tag="264" ind1=" " ind2="1"><subfield code="c">2019</subfield></datafield><datafield tag="336" ind1=" " ind2=" "><subfield code="a">nicht spezifiziert</subfield><subfield code="b">zzz</subfield><subfield code="2">rdacontent</subfield></datafield><datafield tag="337" ind1=" " ind2=" "><subfield code="a">Computermedien</subfield><subfield code="b">c</subfield><subfield code="2">rdamedia</subfield></datafield><datafield tag="338" ind1=" " ind2=" "><subfield code="a">Online-Ressource</subfield><subfield code="b">cr</subfield><subfield code="2">rdacarrier</subfield></datafield><datafield tag="520" ind1=" " ind2=" "><subfield code="a">Lateral control during aircraft-on-ground deceleration, which is one of the most important issues in aircraft-on-ground maneuvers, is discussed in this paper. Based on linear quadratic and predictive control theories, two controllers are developed to replace pilot control, which is effective only to a limited level under severe conditions. Particularly, because the aircraft forward speed decreases during deceleration, we propose a novel weighted model predictive control (MPC) method to control this parameter-varying system. Under the same severe conditions, simulation results show different efficiencies for these two controllers and both exhibited better performance than pilot control.</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Aircraft-on-ground</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Lateral dynamics control</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Parameter variation</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Nonlinear system</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Linear quadratic control</subfield></datafield><datafield tag="650" ind1=" " ind2="4"><subfield code="a">Predictive control</subfield></datafield><datafield tag="700" ind1="1" ind2=" "><subfield code="a">Song, Jian</subfield><subfield code="e">verfasserin</subfield><subfield code="4">aut</subfield></datafield><datafield tag="700" ind1="1" ind2=" 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The lateral control during aircraft-on-ground deceleration phases

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