Real Time Linear Simulation and Control for Small Aircraft Turbojet Engine

The performance of the aircraft gas turbine engine requires optimization because it is directly related to overall aircraft performance. In this study, a modified DYNGEN, a nolinear dynamic simulation program with component maps of the small aircraft turbojet engine, was used to predict the overall...

Full description

Saved in:
Bibliographic Details
Published inJournal of mechanical science and technology Vol. 13; no. 9; pp. 656 - 666
Main Authors Kong, Chang Duk, Chung, Suk Choo
Format Journal Article
LanguageEnglish
Published Seoul 대한기계학회 01.09.1999
Springer Nature B.V
Subjects
Online AccessGet full text

Cover

Loading…
Abstract The performance of the aircraft gas turbine engine requires optimization because it is directly related to overall aircraft performance. In this study, a modified DYNGEN, a nolinear dynamic simulation program with component maps of the small aircraft turbojet engine, was used to predict the overall engine performance. Response characteristics of various cases, such as 6%, 5% and 3% rpm step models and the real-time linear model of the interpolation scheme within the operating range were compared. Among them, the real time linear model was selected for the turbojet engine with nonlinear characteristics. Finally control schemes such as PI (Proportional-Integral Controller) and LQR (Linear Quadratic Regulator) were applied to optimize the engine performance. The overshoot of the turbine inlet temperature was effectively eliminated by LQR controller with the proper control gain K.[PUBLICATION ABSTRACT]
AbstractList The performance of the aircraft gas turbine engine requires optimization because it is directly related to overall aircraft performance. In this study, a modified DYNGEN, a nolinear dynamic simulation program with component maps of the small aircraft turbojet engine, was used to predict the overall engine performance. Response characteristics of various cases, such as 6%, 5% and 3% rpm step models and the real-time linear model of the interpolation scheme within the operating range were compared. Among them, the real time linear model was selected for the turbojet engine with nonlinear characteristics. Finally control schemes such as PI (Proportional-Integral Controller) and LQR (Linear Quadratic Regulator) were applied to optimize the engine performance. The overshoot of the turbine inlet temperature was effectively eliminated by LQR controller with the proper control gain K.[PUBLICATION ABSTRACT]
The performance of the aircraft gas turbine engine requires optimization because it is directly related to overall aircraft performance. In this study, a modified DYNGEN, a nolinear dynamic simulation program with component maps of the small aircraft turbojet engine, was used to predict the overall engine performance. Response characteristics of various cases, such as 6%, 5% and 3% rpm step models and the real-time linear model of the interpolation scheme within the operating range were compared. Among them, the real time linear model was selected for the turbojet engine with nonlinear characteristics. Finally control schemes such as PI (Proportional-Integral Controller) and LQR (Linear Quadratic Regulator) were applied to optimize the engine performance. The overshoot of the turbine inlet temperature was effectively eliminated by LQR controller with the proper control gain K.
Author Chang Duk Kong
Suk Choo Chung
Author_xml – sequence: 1
  givenname: Chang Duk
  surname: Kong
  fullname: Kong, Chang Duk
– sequence: 2
  givenname: Suk Choo
  surname: Chung
  fullname: Chung, Suk Choo
BookMark eNpd0E1LAzEQBuAgFWyrF39BQAQRVvO1ye5Ra-sHxYLW85LuTiQlm2h29-C_N6Wi4GkC82SYeSdo5IMHhE4puaKEqOvbBeG0ELmSB2hMSyUzXjAxSm_GZCYKmR-hSddtCclLxukYPb2AdnhtW8BL60FH_GrbweneBo-1b_As-D4Gh01IrVY7h29srKM2PV4PcRO20OO5f09_j9Gh0a6Dk586RW-L-Xr2kC1X94-zm2VWc0b6rK413QhTQm0EF4ZqEGXaWUuiGG-avJYF51QXJVWKgYR0luHNRhegyrwogU_RxX7uRwyfA3R91dquBue0hzB0FZWKCpqm0UTP_tFtGKJP21WUMFIWu7SSutyrOoaui2Cqj2hbHb8SqnaxVn-xJny-x35ICBqrf_Xz6m5OCOeSccW_AQwvddA
CitedBy_id crossref_primary_10_1115_1_1610014
crossref_primary_10_1007_BF02939343
crossref_primary_10_5139_IJASS_2014_15_2_123
crossref_primary_10_1007_s12206_019_0847_3
Cites_doi 10.1115/97-AA-114
10.1115/96-GT-104
10.1115/1.2906159
10.2514/3.19909
10.1115/1.2906568
10.1115/1.3445601
10.1017/S000192400002340X
10.2514/3.8548
10.1115/1.2906157
10.1115/1.2906571
10.1115/1.2906160
10.1115/1.2906847
10.1115/1.2906536
10.2514/3.21350
10.1115/1.2906516
10.1115/96-GT-332
10.1115/1.2906654
ContentType Journal Article
Copyright The Korean Society of Mechanical Engineers (KSME) 1999
Copyright_xml – notice: The Korean Society of Mechanical Engineers (KSME) 1999
DBID DBRKI
TDB
AAYXX
CITATION
7TB
8FD
8FE
8FG
ABJCF
AFKRA
BENPR
BGLVJ
CCPQU
DWQXO
FR3
HCIFZ
L6V
M7S
PQEST
PQQKQ
PQUKI
PRINS
PTHSS
S0W
H8D
L7M
DOI 10.1007/BF03184576
DatabaseName DBPIA - 디비피아
Korean Database (DBpia)
CrossRef
Mechanical & Transportation Engineering Abstracts
Technology Research Database
ProQuest SciTech Collection
ProQuest Technology Collection
Materials Science & Engineering Collection
ProQuest Central
ProQuest Central
Technology Collection
ProQuest One Community College
ProQuest Central Korea
Engineering Research Database
SciTech Premium Collection
ProQuest Engineering Collection
Engineering Database
ProQuest One Academic Eastern Edition (DO NOT USE)
ProQuest One Academic
ProQuest One Academic UKI Edition
ProQuest Central China
Engineering Collection
DELNET Engineering & Technology Collection
Aerospace Database
Advanced Technologies Database with Aerospace
DatabaseTitle CrossRef
Engineering Database
Technology Collection
Technology Research Database
Mechanical & Transportation Engineering Abstracts
ProQuest One Academic Eastern Edition
SciTech Premium Collection
ProQuest One Community College
ProQuest Technology Collection
ProQuest SciTech Collection
ProQuest Central China
ProQuest Central
ProQuest Engineering Collection
ProQuest One Academic UKI Edition
ProQuest Central Korea
ProQuest DELNET Engineering and Technology Collection
Materials Science & Engineering Collection
Engineering Research Database
ProQuest One Academic
Engineering Collection
Aerospace Database
Advanced Technologies Database with Aerospace
DatabaseTitleList Engineering Database
Aerospace Database
Database_xml – sequence: 1
  dbid: 8FG
  name: ProQuest Technology Collection
  url: https://search.proquest.com/technologycollection1
  sourceTypes: Aggregation Database
DeliveryMethod fulltext_linktorsrc
Discipline Engineering
EISSN 1976-3824
EndPage 666
ExternalDocumentID 2690695131
10_1007_BF03184576
NODE00336237
Genre Feature
GroupedDBID .VR
06D
203
29~
2J2
2KG
2LR
30V
408
40D
40E
8FE
8FG
8UJ
95-
95.
95~
96X
AABHQ
ABFTV
ABJOX
ABKCH
ADURQ
ADYFF
AGDGC
AHYZX
AJRNO
ALMA_UNASSIGNED_HOLDINGS
AMKLP
B-.
BA0
BBWZM
BGNMA
DBRKI
GQ7
GW5
HCIFZ
IXC
I~Z
KOV
KVFHK
L6V
M4Y
MA-
MZR
N2Q
NQJWS
NU0
O93
O9G
O9I
O9J
P19
PF0
PT5
QOK
QOS
ROL
RSV
S16
S3B
SAP
SCV
SDH
SHX
SZN
TDB
TSV
TUC
U2A
VC2
Z45
ZZE
~A9
AAYXX
CITATION
-EM
-Y2
.86
0R~
0VY
1N0
29L
2JN
2JY
2KM
2VQ
2~H
4.4
406
5GY
5VS
6NX
7TB
8FD
AAHNG
AAIAL
AAJBT
AAJKR
AANZL
AARHV
AARTL
AAWCG
AAYIU
AAYQN
AAYTO
ABAKF
ABDZT
ABECU
ABFTD
ABJCF
ABJNI
ABMNI
ABMQK
ABQBU
ABSXP
ABTEG
ABTHY
ABTKH
ABTMW
ABXPI
ACAOD
ACBXY
ACGFS
ACHSB
ACHXU
ACIPQ
ACIWK
ACKNC
ACMDZ
ACMLO
ACOKC
ACOMO
ACSNA
ACZOJ
ADHIR
ADINQ
ADKPE
ADRFC
ADTPH
ADZKW
AEBTG
AEFQL
AEGAL
AEJHL
AEJRE
AEKMD
AEMSY
AENEX
AEOHA
AEPYU
AESKC
AETLH
AEVLU
AEXYK
AFBBN
AFGCZ
AFKRA
AFLOW
AFWTZ
AFZKB
AGAYW
AGJBK
AGMZJ
AGQEE
AGQMX
AGRTI
AGWIL
AGWZB
AGYKE
AHBYD
AHKAY
AHSBF
AIAKS
AILAN
AITGF
AJBLW
ALWAN
AMXSW
AMYLF
AOCGG
ARMRJ
AXYYD
AYJHY
BDATZ
BENPR
BGLVJ
CAG
CCPQU
COF
CS3
CSCUP
DDRTE
DNIVK
DPUIP
DWQXO
EBLON
EBS
EIOEI
EJD
ESBYG
FERAY
FFXSO
FIGPU
FINBP
FNLPD
FR3
FRRFC
FSGXE
FWDCC
GGCAI
GGRSB
GJIRD
GNWQR
GQ6
HF~
HG6
HMJXF
HRMNR
HZ~
IJ-
IKXTQ
IWAJR
IXD
J-C
J0Z
JBSCW
JZLTJ
LLZTM
M7S
NPVJJ
O9-
P9P
PQEST
PQQKQ
PQUKI
PRINS
PT4
PTHSS
R89
R9I
RHV
S0W
S27
SEG
SJYHP
SNE
SNPRN
SNX
SOHCF
SOJ
SPISZ
SRMVM
SSLCW
T13
TSG
UG4
UOJIU
UTJUX
UZXMN
VFIZW
WK8
YLTOR
Z7R
Z7V
Z7W
Z7X
Z7Y
Z7Z
Z81
Z83
Z85
Z88
ZMTXR
AATNV
ABFGW
ACWMK
AESTI
AEVTX
AIMYW
AKQUC
H8D
L7M
UNUBA
ID FETCH-LOGICAL-c320t-cca1b4f9ecf434f1ae49318a60723dd5c68331a891772e6e007f3dba8e79589e3
IEDL.DBID 8FG
ISSN 1226-4865
1738-494X
IngestDate Sat Aug 17 03:55:37 EDT 2024
Fri Sep 13 07:38:16 EDT 2024
Fri Aug 23 00:33:55 EDT 2024
Tue Sep 17 19:40:12 EDT 2024
IsPeerReviewed true
IsScholarly true
Issue 9
Language English
LinkModel DirectLink
MergedId FETCHMERGED-LOGICAL-c320t-cca1b4f9ecf434f1ae49318a60723dd5c68331a891772e6e007f3dba8e79589e3
Notes ObjectType-Article-1
SourceType-Scholarly Journals-1
ObjectType-Feature-2
content type line 23
PQID 1020980318
PQPubID 326249
PageCount 11
ParticipantIDs proquest_miscellaneous_1671410721
proquest_journals_1020980318
crossref_primary_10_1007_BF03184576
nurimedia_primary_NODE00336237
PublicationCentury 1900
PublicationDate 1999-09-01
PublicationDateYYYYMMDD 1999-09-01
PublicationDate_xml – month: 09
  year: 1999
  text: 1999-09-01
  day: 01
PublicationDecade 1990
PublicationPlace Seoul
PublicationPlace_xml – name: Seoul
PublicationTitle Journal of mechanical science and technology
PublicationYear 1999
Publisher 대한기계학회
Springer Nature B.V
Publisher_xml – name: 대한기계학회
– name: Springer Nature B.V
References A. Stamatis (BF03184576_CR17) 1990; 112
J. R. Mihaloew (BF03184576_CR11) 1984; 7
BF03184576_CR21
I. H. Ismail (BF03184576_CR7) 1991; 113
Y. Wang (BF03184576_CR19) 1991; 113
J. W. Watts (BF03184576_CR20) 1992; 114
D, L Smith (BF03184576_CR15) 1990; 112
L. J. Kerr (BF03184576_CR5) 1992; 114
D. L Smith (BF03184576_CR16) 1990; 112
N. Sugiyama (BF03184576_CR18) 1994; 17
C. D. Kong (BF03184576_CR6) 1995; 23
Z. Ping (BF03184576_CR12) 1992; 114
BF03184576_CR8
BF03184576_CR9
BF03184576_CR4
M. T. Schobeiri (BF03184576_CR13) 1994; 116
BF03184576_CR2
BF03184576_CR3
BF03184576_CR14
W. Merrill (BF03184576_CR10) 1984; 7
BF03184576_CR1
References_xml – ident: BF03184576_CR21
  doi: 10.1115/97-AA-114
– ident: BF03184576_CR14
– ident: BF03184576_CR3
  doi: 10.1115/96-GT-104
– volume: 112
  start-page: 182
  year: 1990
  ident: BF03184576_CR16
  publication-title: J. of Eng. for Gas Turbines and Power
  doi: 10.1115/1.2906159
  contributor:
    fullname: D. L Smith
– volume: 7
  start-page: 652
  issue: No. 6
  year: 1984
  ident: BF03184576_CR10
  publication-title: J. of Guidance
  doi: 10.2514/3.19909
  contributor:
    fullname: W. Merrill
– volume: 114
  start-page: 180
  year: 1992
  ident: BF03184576_CR12
  publication-title: J. of Gas Turbines and Power
  doi: 10.1115/1.2906568
  contributor:
    fullname: Z. Ping
– ident: BF03184576_CR2
  doi: 10.1115/1.3445601
– ident: BF03184576_CR8
  doi: 10.1017/S000192400002340X
– ident: BF03184576_CR9
– volume: 7
  start-page: 77
  issue: No. 1
  year: 1984
  ident: BF03184576_CR11
  publication-title: J. of Guidance
  doi: 10.2514/3.8548
  contributor:
    fullname: J. R. Mihaloew
– ident: BF03184576_CR4
– volume: 112
  start-page: 168
  year: 1990
  ident: BF03184576_CR17
  publication-title: J. of Eng. for Gas Turbines and Power
  doi: 10.1115/1.2906157
  contributor:
    fullname: A. Stamatis
– volume: 114
  start-page: 187
  year: 1992
  ident: BF03184576_CR5
  publication-title: J. of Eng. for Gas Turbines and Power
  doi: 10.1115/1.2906571
  contributor:
    fullname: L. J. Kerr
– volume: 112
  start-page: 187
  year: 1990
  ident: BF03184576_CR15
  publication-title: J. of Eng. for Gas Turbines and Power
  doi: 10.1115/1.2906160
  contributor:
    fullname: D, L Smith
– volume: 116
  start-page: 483
  year: 1994
  ident: BF03184576_CR13
  publication-title: J. of Gas Turbines and Power
  doi: 10.1115/1.2906847
  contributor:
    fullname: M. T. Schobeiri
– volume: 23
  start-page: 9
  year: 1995
  ident: BF03184576_CR6
  publication-title: J. of KSAS
  contributor:
    fullname: C. D. Kong
– volume: 113
  start-page: 95
  year: 1991
  ident: BF03184576_CR7
  publication-title: J. of Eng. for Gas Turbines and Power
  doi: 10.1115/1.2906536
  contributor:
    fullname: I. H. Ismail
– volume: 17
  start-page: 1320
  issue: NO. 6
  year: 1994
  ident: BF03184576_CR18
  publication-title: J. of Guidance
  doi: 10.2514/3.21350
  contributor:
    fullname: N. Sugiyama
– volume: 113
  start-page: 106
  year: 1991
  ident: BF03184576_CR19
  publication-title: J. of Eng. for Gas Turbines and Power
  doi: 10.1115/1.2906516
  contributor:
    fullname: Y. Wang
– ident: BF03184576_CR1
  doi: 10.1115/96-GT-332
– volume: 114
  start-page: 763
  year: 1992
  ident: BF03184576_CR20
  publication-title: J. of Eng. for Gas Turbines and Power
  doi: 10.1115/1.2906654
  contributor:
    fullname: J. W. Watts
SSID ssj0059231
ssj0062411
Score 1.5527676
Snippet The performance of the aircraft gas turbine engine requires optimization because it is directly related to overall aircraft performance. In this study, a...
SourceID proquest
crossref
nurimedia
SourceType Aggregation Database
Publisher
StartPage 656
SubjectTerms Aerospace engines
Aircraft
Aircraft components
Computer simulation
Gas turbine engines
Nonlinearity
R&D
Real time
Research & development
Studies
Turbojet engines
Title Real Time Linear Simulation and Control for Small Aircraft Turbojet Engine
URI https://www.dbpia.co.kr/journal/articleDetail?nodeId=NODE00336237
https://www.proquest.com/docview/1020980318/abstract/
https://search.proquest.com/docview/1671410721
Volume 13
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
link http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV3dS8MwED_8eFAfxE-czhHR1-K6pknzJJtuDsEporC3cWlTmGinW_f_e9e1UxF8KqEhkLvkfpfk7ncAFwTZCUYu9RKLoSdj9D2bUNNpS-gcIKESJwrfD1T_Rd4Nw-EK9KtcGA6rrGxiYaiTScx35LS7W00T8RK8RMu3AHF-efXx6XH9KH5nLYtprMK6z5x4nDPeu61ssiKcKo5emra3NHL4m6iUBpUhs478gKaNbM78-qSkP1a6gJ7eDmyXPqNoL5S8Cysu24OtH0yC-3D3RA6f4ELxgv1GnIrZ-L2szCUwS0QZki7IRxWzd3x7EziexlNMc0GgYyevLheuGPEAXnrd5-u-V5ZJ8OKg1cw90oFvZWpcnMpApj46aWhGqJq6FSRJGKsoCHyM6GCmW045mnQakGoip00YGRccwlo2ydwRCMkJg6h9X8VaJsYaZY0fKdRhqB2GqgbnlYRGHws2jFHFe_wtxxo0lsJbdhs83HS5cBy5W7oG9Uqio3LLzEbfCq7B2fI3LXZ-wcDMTebUR2mOS6VT6_H_Q5zA5oJfgYPB6rCWT-fulLyH3DaKhdGA9Xav0xnQt9MdPD59Aa73xfU
link.rule.ids 315,786,790,12792,21416,27957,27958,33408,33779,33780,43635,43840,74392,74659
linkProvider ProQuest
linkToHtml http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV3fT8IwEL4oPqAPxp8RRazR1yWMdu36ZIyCiICJwYS3pdu6BAMbsvH_ex0bYEx8XNZc0rv2vmt79x3APUJ2qFwdWaGvHIsFyrb8ED-18BGdqUJUMoXCgyHvfrLe2BkXF25pkVZZ-sTcUYdJYO7IcXe3mtI1S_Bh_m2ZrlHmdbVoobELe4widJpK8c5L6Yk5olN-4BK4qZlk49_0pCiKOYZrZAuQqvHSsOqjaf745hxwOkdwWESK5HFl2mPY0fEJHGzxB55C7wPDPGLawxMTLaoFSSezoh8XUXFIikR0gpEpSWdqOiVqsggWKsoIQo2ffOmM6FziGXx22qOnrlU0R7AC2mpmFmre9lkkdRAxyiJbaSZxRoo3RYuGoRNwl1JbuXgcEy3NNU46omgQVwvpuFLTc6jESawvgDBTJqiEbfNAsFD6kvvSdrkSjiO0cngN7koNefMVB4ZXsh1v9FiDxlp562HD9-e2aReHQZaoQb3UqFdslNTbmLUGt-vfuMTNu4WKdbLEMVyYbFQ8q17-L-IGqt3RoO_1X4dvV7C_Ylgw6WB1qGSLpb7G-CHzG_ki-QH_vMIN
linkToPdf http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV3dS8MwED90gh8P4idOp0b0tbiu-WiexI-NOXWOobC3krYpTGana_f_e-nSbSL4WBIOcne536W5_A7gCiE7Vr5OnDhUzKGRcp0wxk8tQkRnTyEqmYfCL13efqedARvY-qfMllWWMbEI1PE4Mv_IcXc36tI3Lnid2LKI3kPr5uvbMR2kzE2rbaexCmuCcoYevnbX7Pb6ZVzmiFXF8UvgFqeSDn6TlaJgygzzyBI8baRTw7GPhvoTqQv4ae3Ats0bye3M0LuwotM92FpiE9yHTh-TPmKaxROTO6oJyYaftjsXUWlMbFk6wTyVZJ9qNCJqOIkmKskJAk84_tA50YXEA3hvNd_u245tleBEXqOeO2gHN6SJ1FFCPZq4SlOJK1K8LhpeHLOI-57nKh8PZ6KhucZFJx6ax9dCMl9q7xAq6TjVR0CoeTSohOvySNBYhpKH0vW5EowJrRivwmWpoeBrxogRlNzHCz1W4WyuvPm07utD0zSPw5RLVKFWajSw2yYLFkauwsV8GB3e3GKoVI-nOIcLU5uKJ9fj_0Wcwzp6SPD82H06gc0Z3YKpDatBJZ9M9SkmE3l4Zr3kB3vYx7A
openUrl ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Ajournal&rft.genre=article&rft.atitle=Real+time+linear+simulation+and+control+for+small+aircraft+turbojet+engine&rft.jtitle=Journal+of+mechanical+science+and+technology&rft.au=Kong%2C+Chang+Duk&rft.au=Chung%2C+Suk+Choo&rft.date=1999-09-01&rft.issn=1738-494X&rft.volume=13&rft.issue=9&rft.spage=656&rft.epage=666&rft_id=info:doi/10.1007%2FBF03184576&rft.externalDBID=NO_FULL_TEXT
thumbnail_l http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1226-4865&client=summon
thumbnail_m http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1226-4865&client=summon
thumbnail_s http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1226-4865&client=summon