Flying qualities evaluation based nonlinear flight control law design method for aircraft

This paper is focused on the parameter tuning problem for the design of nonlinear flight controllers. Taking into account the preferences and requirements of the pilot, a novel flying qualities evaluation framework and a tuning method are proposed for the design of nonlinear flight controllers. Cons...
Ausführliche Beschreibung

Gespeichert in:

Autor*in:	Sun, Liguo [verfasserIn] Shi, Lewen [verfasserIn] Tan, Wenqian [verfasserIn] Liu, Xiaoyu [verfasserIn]

Format:	E-Artikel
Sprache:	Englisch

Erschienen:	2020

Schlagwörter:	Flight control Nonlinear control Flying qualities criteria Controller design

Übergeordnetes Werk:	Enthalten in: Aerospace science and technology - Amsterdam [u.a.] : Elsevier Science, 1997, 106
Übergeordnetes Werk:	volume:106

DOI / URN:	10.1016/j.ast.2020.106126

Katalog-ID:	ELV004836014

Internformat


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245	1	0	\|a Flying qualities evaluation based nonlinear flight control law design method for aircraft
264		1	\|c 2020
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337			\|a Computermedien \|b c \|2 rdamedia
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520			\|a This paper is focused on the parameter tuning problem for the design of nonlinear flight controllers. Taking into account the preferences and requirements of the pilot, a novel flying qualities evaluation framework and a tuning method are proposed for the design of nonlinear flight controllers. Considering that the existing flying qualities criteria are not applicable to evaluating the closed-loop aircraft system, a novel evaluation framework consisting of three modules namely ideal reference model, controller and aircraft model, is proposed. Based on this evaluation framework, an overall evaluation model is established, the flying qualities based rating scores for this model will reflect the level of the controller performance. Subsequently, a schematic evaluation method, consisting of three sub-procedures namely linearization, low-order equivalent fitting and flying qualities criteria based rating, is proposed for the controller design. To validate the evaluation framework and the method, a nonlinear F/A-18 aircraft model and the incremental backstepping control law are chosen to build a demonstration example. Theoretical analysis and the simulation results reveal that the proposed evaluation framework and schematic method are effective for the design of nonlinear flight control laws.
650		4	\|a Flight control
650		4	\|a Nonlinear control
650		4	\|a Flying qualities criteria
650		4	\|a Controller design
700	1		\|a Shi, Lewen \|e verfasserin \|4 aut
700	1		\|a Tan, Wenqian \|e verfasserin \|4 aut
700	1		\|a Liu, Xiaoyu \|e verfasserin \|0 (orcid)0000-0002-5200-9563 \|4 aut
773	0	8	\|i Enthalten in \|t Aerospace science and technology \|d Amsterdam [u.a.] : Elsevier Science, 1997 \|g 106 \|h Online-Ressource \|w (DE-627)320521486 \|w (DE-600)2014638-3 \|w (DE-576)255630425 \|x 1626-3219 \|7 nnns
773	1	8	\|g volume:106
912			\|a GBV_USEFLAG_U
912			\|a SYSFLAG_U
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912			\|a GBV_ILN_22
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912			\|a GBV_ILN_31
912			\|a GBV_ILN_32
912			\|a GBV_ILN_40
912			\|a GBV_ILN_60
912			\|a GBV_ILN_62
912			\|a GBV_ILN_63
912			\|a GBV_ILN_65
912			\|a GBV_ILN_69
912			\|a GBV_ILN_70
912			\|a GBV_ILN_73
912			\|a GBV_ILN_74
912			\|a GBV_ILN_90
912			\|a GBV_ILN_95
912			\|a GBV_ILN_100
912			\|a GBV_ILN_105
912			\|a GBV_ILN_110
912			\|a GBV_ILN_150
912			\|a GBV_ILN_151
912			\|a GBV_ILN_224
912			\|a GBV_ILN_370
912			\|a GBV_ILN_602
912			\|a GBV_ILN_702
912			\|a GBV_ILN_2003
912			\|a GBV_ILN_2004
912			\|a GBV_ILN_2005
912			\|a GBV_ILN_2006
912			\|a GBV_ILN_2008
912			\|a GBV_ILN_2011
912			\|a GBV_ILN_2014
912			\|a GBV_ILN_2015
912			\|a GBV_ILN_2020
912			\|a GBV_ILN_2021
912			\|a GBV_ILN_2025
912			\|a GBV_ILN_2027
912			\|a GBV_ILN_2034
912			\|a GBV_ILN_2038
912			\|a GBV_ILN_2044
912			\|a GBV_ILN_2048
912			\|a GBV_ILN_2049
912			\|a GBV_ILN_2050
912			\|a GBV_ILN_2056
912			\|a GBV_ILN_2059
912			\|a GBV_ILN_2061
912			\|a GBV_ILN_2064
912			\|a GBV_ILN_2065
912			\|a GBV_ILN_2068
912			\|a GBV_ILN_2088
912			\|a GBV_ILN_2111
912			\|a GBV_ILN_2112
912			\|a GBV_ILN_2113
912			\|a GBV_ILN_2118
912			\|a GBV_ILN_2122
912			\|a GBV_ILN_2129
912			\|a GBV_ILN_2143
912			\|a GBV_ILN_2147
912			\|a GBV_ILN_2148
912			\|a GBV_ILN_2152
912			\|a GBV_ILN_2153
912			\|a GBV_ILN_2190
912			\|a GBV_ILN_2336
912			\|a GBV_ILN_2470
912			\|a GBV_ILN_2507
912			\|a GBV_ILN_2522
912			\|a GBV_ILN_4035
912			\|a GBV_ILN_4037
912			\|a GBV_ILN_4046
912			\|a GBV_ILN_4112
912			\|a GBV_ILN_4125
912			\|a GBV_ILN_4126
912			\|a GBV_ILN_4242
912			\|a GBV_ILN_4251
912			\|a GBV_ILN_4305
912			\|a GBV_ILN_4313
912			\|a GBV_ILN_4322
912			\|a GBV_ILN_4323
912			\|a GBV_ILN_4324
912			\|a GBV_ILN_4325
912			\|a GBV_ILN_4326
912			\|a GBV_ILN_4333
912			\|a GBV_ILN_4334
912			\|a GBV_ILN_4335
912			\|a GBV_ILN_4338
912			\|a GBV_ILN_4393
936	b	k	\|a 55.50 \|j Luftfahrzeugtechnik
936	b	k	\|a 55.60 \|j Raumfahrttechnik
936	b	k	\|a 55.60 \|j Raumfahrttechnik
951			\|a AR
952			\|d 106

Indexfelder

author_variant	l s ls l s ls w t wt x l xl
matchkey_str	article:16263219:2020----::ligulteeautobsdolnafihcnrlad
hierarchy_sort_str	2020
bklnumber	55.50 55.60
publishDate	2020
allfields	10.1016/j.ast.2020.106126 doi (DE-627)ELV004836014 (ELSEVIER)S1270-9638(20)30808-7 DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Sun, Liguo verfasserin aut Flying qualities evaluation based nonlinear flight control law design method for aircraft 2020 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper is focused on the parameter tuning problem for the design of nonlinear flight controllers. Taking into account the preferences and requirements of the pilot, a novel flying qualities evaluation framework and a tuning method are proposed for the design of nonlinear flight controllers. Considering that the existing flying qualities criteria are not applicable to evaluating the closed-loop aircraft system, a novel evaluation framework consisting of three modules namely ideal reference model, controller and aircraft model, is proposed. Based on this evaluation framework, an overall evaluation model is established, the flying qualities based rating scores for this model will reflect the level of the controller performance. Subsequently, a schematic evaluation method, consisting of three sub-procedures namely linearization, low-order equivalent fitting and flying qualities criteria based rating, is proposed for the controller design. To validate the evaluation framework and the method, a nonlinear F/A-18 aircraft model and the incremental backstepping control law are chosen to build a demonstration example. Theoretical analysis and the simulation results reveal that the proposed evaluation framework and schematic method are effective for the design of nonlinear flight control laws. Flight control Nonlinear control Flying qualities criteria Controller design Shi, Lewen verfasserin aut Tan, Wenqian verfasserin aut Liu, Xiaoyu verfasserin (orcid)0000-0002-5200-9563 aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 106 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:106 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 106
spelling	10.1016/j.ast.2020.106126 doi (DE-627)ELV004836014 (ELSEVIER)S1270-9638(20)30808-7 DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Sun, Liguo verfasserin aut Flying qualities evaluation based nonlinear flight control law design method for aircraft 2020 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper is focused on the parameter tuning problem for the design of nonlinear flight controllers. Taking into account the preferences and requirements of the pilot, a novel flying qualities evaluation framework and a tuning method are proposed for the design of nonlinear flight controllers. Considering that the existing flying qualities criteria are not applicable to evaluating the closed-loop aircraft system, a novel evaluation framework consisting of three modules namely ideal reference model, controller and aircraft model, is proposed. Based on this evaluation framework, an overall evaluation model is established, the flying qualities based rating scores for this model will reflect the level of the controller performance. Subsequently, a schematic evaluation method, consisting of three sub-procedures namely linearization, low-order equivalent fitting and flying qualities criteria based rating, is proposed for the controller design. To validate the evaluation framework and the method, a nonlinear F/A-18 aircraft model and the incremental backstepping control law are chosen to build a demonstration example. Theoretical analysis and the simulation results reveal that the proposed evaluation framework and schematic method are effective for the design of nonlinear flight control laws. Flight control Nonlinear control Flying qualities criteria Controller design Shi, Lewen verfasserin aut Tan, Wenqian verfasserin aut Liu, Xiaoyu verfasserin (orcid)0000-0002-5200-9563 aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 106 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:106 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 106
allfields_unstemmed	10.1016/j.ast.2020.106126 doi (DE-627)ELV004836014 (ELSEVIER)S1270-9638(20)30808-7 DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Sun, Liguo verfasserin aut Flying qualities evaluation based nonlinear flight control law design method for aircraft 2020 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper is focused on the parameter tuning problem for the design of nonlinear flight controllers. Taking into account the preferences and requirements of the pilot, a novel flying qualities evaluation framework and a tuning method are proposed for the design of nonlinear flight controllers. Considering that the existing flying qualities criteria are not applicable to evaluating the closed-loop aircraft system, a novel evaluation framework consisting of three modules namely ideal reference model, controller and aircraft model, is proposed. Based on this evaluation framework, an overall evaluation model is established, the flying qualities based rating scores for this model will reflect the level of the controller performance. Subsequently, a schematic evaluation method, consisting of three sub-procedures namely linearization, low-order equivalent fitting and flying qualities criteria based rating, is proposed for the controller design. To validate the evaluation framework and the method, a nonlinear F/A-18 aircraft model and the incremental backstepping control law are chosen to build a demonstration example. Theoretical analysis and the simulation results reveal that the proposed evaluation framework and schematic method are effective for the design of nonlinear flight control laws. Flight control Nonlinear control Flying qualities criteria Controller design Shi, Lewen verfasserin aut Tan, Wenqian verfasserin aut Liu, Xiaoyu verfasserin (orcid)0000-0002-5200-9563 aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 106 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:106 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 106
allfieldsGer	10.1016/j.ast.2020.106126 doi (DE-627)ELV004836014 (ELSEVIER)S1270-9638(20)30808-7 DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Sun, Liguo verfasserin aut Flying qualities evaluation based nonlinear flight control law design method for aircraft 2020 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper is focused on the parameter tuning problem for the design of nonlinear flight controllers. Taking into account the preferences and requirements of the pilot, a novel flying qualities evaluation framework and a tuning method are proposed for the design of nonlinear flight controllers. Considering that the existing flying qualities criteria are not applicable to evaluating the closed-loop aircraft system, a novel evaluation framework consisting of three modules namely ideal reference model, controller and aircraft model, is proposed. Based on this evaluation framework, an overall evaluation model is established, the flying qualities based rating scores for this model will reflect the level of the controller performance. Subsequently, a schematic evaluation method, consisting of three sub-procedures namely linearization, low-order equivalent fitting and flying qualities criteria based rating, is proposed for the controller design. To validate the evaluation framework and the method, a nonlinear F/A-18 aircraft model and the incremental backstepping control law are chosen to build a demonstration example. Theoretical analysis and the simulation results reveal that the proposed evaluation framework and schematic method are effective for the design of nonlinear flight control laws. Flight control Nonlinear control Flying qualities criteria Controller design Shi, Lewen verfasserin aut Tan, Wenqian verfasserin aut Liu, Xiaoyu verfasserin (orcid)0000-0002-5200-9563 aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 106 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:106 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 106
allfieldsSound	10.1016/j.ast.2020.106126 doi (DE-627)ELV004836014 (ELSEVIER)S1270-9638(20)30808-7 DE-627 ger DE-627 rda eng 620 DE-600 55.50 bkl 55.60 bkl 55.60 bkl Sun, Liguo verfasserin aut Flying qualities evaluation based nonlinear flight control law design method for aircraft 2020 nicht spezifiziert zzz rdacontent Computermedien c rdamedia Online-Ressource cr rdacarrier This paper is focused on the parameter tuning problem for the design of nonlinear flight controllers. Taking into account the preferences and requirements of the pilot, a novel flying qualities evaluation framework and a tuning method are proposed for the design of nonlinear flight controllers. Considering that the existing flying qualities criteria are not applicable to evaluating the closed-loop aircraft system, a novel evaluation framework consisting of three modules namely ideal reference model, controller and aircraft model, is proposed. Based on this evaluation framework, an overall evaluation model is established, the flying qualities based rating scores for this model will reflect the level of the controller performance. Subsequently, a schematic evaluation method, consisting of three sub-procedures namely linearization, low-order equivalent fitting and flying qualities criteria based rating, is proposed for the controller design. To validate the evaluation framework and the method, a nonlinear F/A-18 aircraft model and the incremental backstepping control law are chosen to build a demonstration example. Theoretical analysis and the simulation results reveal that the proposed evaluation framework and schematic method are effective for the design of nonlinear flight control laws. Flight control Nonlinear control Flying qualities criteria Controller design Shi, Lewen verfasserin aut Tan, Wenqian verfasserin aut Liu, Xiaoyu verfasserin (orcid)0000-0002-5200-9563 aut Enthalten in Aerospace science and technology Amsterdam [u.a.] : Elsevier Science, 1997 106 Online-Ressource (DE-627)320521486 (DE-600)2014638-3 (DE-576)255630425 1626-3219 nnns volume:106 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 106
language	English
source	Enthalten in Aerospace science and technology 106 volume:106
sourceStr	Enthalten in Aerospace science and technology 106 volume:106
format_phy_str_mv	Article
bklname	Luftfahrzeugtechnik Raumfahrttechnik
institution	findex.gbv.de
topic_facet	Flight control Nonlinear control Flying qualities criteria Controller design
dewey-raw	620
isfreeaccess_bool	false
container_title	Aerospace science and technology
authorswithroles_txt_mv	Sun, Liguo @@aut@@ Shi, Lewen @@aut@@ Tan, Wenqian @@aut@@ Liu, Xiaoyu @@aut@@
publishDateDaySort_date	2020-01-01T00:00:00Z
hierarchy_top_id	320521486
dewey-sort	3620
id	ELV004836014
language_de	englisch
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author	Sun, Liguo
spellingShingle	Sun, Liguo ddc 620 bkl 55.50 bkl 55.60 misc Flight control misc Nonlinear control misc Flying qualities criteria misc Controller design Flying qualities evaluation based nonlinear flight control law design method for aircraft
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topic_title	620 DE-600 55.50 bkl 55.60 bkl Flying qualities evaluation based nonlinear flight control law design method for aircraft Flight control Nonlinear control Flying qualities criteria Controller design
topic	ddc 620 bkl 55.50 bkl 55.60 misc Flight control misc Nonlinear control misc Flying qualities criteria misc Controller design
topic_unstemmed	ddc 620 bkl 55.50 bkl 55.60 misc Flight control misc Nonlinear control misc Flying qualities criteria misc Controller design
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format_facet	Elektronische Aufsätze Aufsätze Elektronische Ressource
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title	Flying qualities evaluation based nonlinear flight control law design method for aircraft
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title_full	Flying qualities evaluation based nonlinear flight control law design method for aircraft
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author_browse	Sun, Liguo Shi, Lewen Tan, Wenqian Liu, Xiaoyu
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title_sort	flying qualities evaluation based nonlinear flight control law design method for aircraft
title_auth	Flying qualities evaluation based nonlinear flight control law design method for aircraft
abstract	This paper is focused on the parameter tuning problem for the design of nonlinear flight controllers. Taking into account the preferences and requirements of the pilot, a novel flying qualities evaluation framework and a tuning method are proposed for the design of nonlinear flight controllers. Considering that the existing flying qualities criteria are not applicable to evaluating the closed-loop aircraft system, a novel evaluation framework consisting of three modules namely ideal reference model, controller and aircraft model, is proposed. Based on this evaluation framework, an overall evaluation model is established, the flying qualities based rating scores for this model will reflect the level of the controller performance. Subsequently, a schematic evaluation method, consisting of three sub-procedures namely linearization, low-order equivalent fitting and flying qualities criteria based rating, is proposed for the controller design. To validate the evaluation framework and the method, a nonlinear F/A-18 aircraft model and the incremental backstepping control law are chosen to build a demonstration example. Theoretical analysis and the simulation results reveal that the proposed evaluation framework and schematic method are effective for the design of nonlinear flight control laws.
abstractGer	This paper is focused on the parameter tuning problem for the design of nonlinear flight controllers. Taking into account the preferences and requirements of the pilot, a novel flying qualities evaluation framework and a tuning method are proposed for the design of nonlinear flight controllers. Considering that the existing flying qualities criteria are not applicable to evaluating the closed-loop aircraft system, a novel evaluation framework consisting of three modules namely ideal reference model, controller and aircraft model, is proposed. Based on this evaluation framework, an overall evaluation model is established, the flying qualities based rating scores for this model will reflect the level of the controller performance. Subsequently, a schematic evaluation method, consisting of three sub-procedures namely linearization, low-order equivalent fitting and flying qualities criteria based rating, is proposed for the controller design. To validate the evaluation framework and the method, a nonlinear F/A-18 aircraft model and the incremental backstepping control law are chosen to build a demonstration example. Theoretical analysis and the simulation results reveal that the proposed evaluation framework and schematic method are effective for the design of nonlinear flight control laws.
abstract_unstemmed	This paper is focused on the parameter tuning problem for the design of nonlinear flight controllers. Taking into account the preferences and requirements of the pilot, a novel flying qualities evaluation framework and a tuning method are proposed for the design of nonlinear flight controllers. Considering that the existing flying qualities criteria are not applicable to evaluating the closed-loop aircraft system, a novel evaluation framework consisting of three modules namely ideal reference model, controller and aircraft model, is proposed. Based on this evaluation framework, an overall evaluation model is established, the flying qualities based rating scores for this model will reflect the level of the controller performance. Subsequently, a schematic evaluation method, consisting of three sub-procedures namely linearization, low-order equivalent fitting and flying qualities criteria based rating, is proposed for the controller design. To validate the evaluation framework and the method, a nonlinear F/A-18 aircraft model and the incremental backstepping control law are chosen to build a demonstration example. Theoretical analysis and the simulation results reveal that the proposed evaluation framework and schematic method are effective for the design of nonlinear flight control laws.
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title_short	Flying qualities evaluation based nonlinear flight control law design method for aircraft
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author2	Shi, Lewen Tan, Wenqian Liu, Xiaoyu
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doi_str	10.1016/j.ast.2020.106126
up_date	2024-07-07T00:18:35.219Z
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Flying qualities evaluation based nonlinear flight control law design method for aircraft

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