Active-set pseudospectral model predictive static programming for midcourse guidance

This paper focuses on the midcourse guidance law for the interceptor to engage the hypersonic gliding vehicles (HGVs). Firstly, an active-set pseudospectral model predictive static programming (APS-MPSP) algorithm is presented, which entails two major improvements: the application of pseudospectral...

Celý popis

Uložené v:
Podrobná bibliografia
Vydané v:Aerospace science and technology Ročník 134; s. 108137
Hlavní autori: Zhou, Cong, He, Lei, Yan, Xiaodong, Meng, Fanqin, Li, Chaoyong
Médium: Journal Article
Jazyk:English
Vydavateľské údaje: Elsevier Masson SAS 01.03.2023
Predmet:
ISSN:1270-9638, 1626-3219
On-line prístup:Získať plný text
Tagy: Pridať tag
Žiadne tagy, Buďte prvý, kto otaguje tento záznam!
Abstract This paper focuses on the midcourse guidance law for the interceptor to engage the hypersonic gliding vehicles (HGVs). Firstly, an active-set pseudospectral model predictive static programming (APS-MPSP) algorithm is presented, which entails two major improvements: the application of pseudospectral discretion and handling of control constraint using active-set iteration strategy. Except inheriting the high efficiency of the MPSP, this new algorithm can address the control constraint directly. Secondly, the optimal predictive guidance design is established, which embeds the target prediction into the guidance framework by formulating a simultaneous nonlinear optimal problem. Employing the APS-MPSP algorithm to solve this optimal problem efficiently, the predictive guidance command that ensures interceptor reach an appropriate predicted interception point (PIP) can be obtained directly. This strategy has the merits of no need to precompute the PIP or time-to-go and high prediction accuracy. The reliability and efficiency of the proposed methods are verified by numerical examples and comparisons with already methods.
AbstractList This paper focuses on the midcourse guidance law for the interceptor to engage the hypersonic gliding vehicles (HGVs). Firstly, an active-set pseudospectral model predictive static programming (APS-MPSP) algorithm is presented, which entails two major improvements: the application of pseudospectral discretion and handling of control constraint using active-set iteration strategy. Except inheriting the high efficiency of the MPSP, this new algorithm can address the control constraint directly. Secondly, the optimal predictive guidance design is established, which embeds the target prediction into the guidance framework by formulating a simultaneous nonlinear optimal problem. Employing the APS-MPSP algorithm to solve this optimal problem efficiently, the predictive guidance command that ensures interceptor reach an appropriate predicted interception point (PIP) can be obtained directly. This strategy has the merits of no need to precompute the PIP or time-to-go and high prediction accuracy. The reliability and efficiency of the proposed methods are verified by numerical examples and comparisons with already methods.
ArticleNumber 108137
Author Meng, Fanqin
He, Lei
Li, Chaoyong
Yan, Xiaodong
Zhou, Cong
Author_xml – sequence: 1
  givenname: Cong
  orcidid: 0000-0003-1667-212X
  surname: Zhou
  fullname: Zhou, Cong
  email: zhoucongnwpu@163.com
  organization: School of Astronautics, Northwestern Polytechnical University, Xi'an, Shaanxi, 710072, China
– sequence: 2
  givenname: Lei
  orcidid: 0000-0001-7056-5902
  surname: He
  fullname: He, Lei
  email: helei0728@mail.nwpu.edu.cn
  organization: Beijing Institute of Astronautical Systems Engineering, Beijing, 100076, China
– sequence: 3
  givenname: Xiaodong
  orcidid: 0000-0002-2282-6001
  surname: Yan
  fullname: Yan, Xiaodong
  email: yan804@nwpu.edu.cn
  organization: School of Astronautics, Northwestern Polytechnical University, Xi'an, Shaanxi, 710072, China
– sequence: 4
  givenname: Fanqin
  orcidid: 0000-0002-8388-7588
  surname: Meng
  fullname: Meng, Fanqin
  email: mfqgnn@hotmail.com
  organization: School of Astronautics, Northwestern Polytechnical University, Xi'an, Shaanxi, 710072, China
– sequence: 5
  givenname: Chaoyong
  surname: Li
  fullname: Li, Chaoyong
  email: Chaoyong@zju.edu.cn
  organization: College of Electrical Engineering, Zhejiang University, Hangzhou, 310027, China
BookMark eNp9kMtqAjEUhkOxULV9gO7yAmNzGTMTuhLpDYRu7DrE5EQiM5MhiULfvrF21YWrc-F8B_5vhiZDGAChR0oWlFDxdFjolBeMMF7mlvLmBk2pYKLijMpJ6VlDKil4e4dmKR0IIUzWbIq2K5P9CaoEGY8JjjakEUyOusN9sNDhMYL1vzc4ZZ29KZuwj7rv_bDHLkTce2vCMSbA-6O3ejBwj26d7hI8_NU5-np92a7fq83n28d6takMY02udtJxJqXhra0Z6LYp007vjLNLbgWhZWMpc8a00hpHuW20WC5rJlgNljrJ54he_poYUorg1Bh9r-O3okSdtaiDKlrUWYu6aClM848x_pwrDCW0766SzxcSSqSTh6iS8VDiWh-LMmWDv0L_AL2ygQ4
CitedBy_id crossref_primary_10_3390_aerospace12070610
crossref_primary_10_1016_j_cja_2024_08_029
crossref_primary_10_1016_j_cja_2024_08_030
crossref_primary_10_1016_j_ast_2025_109960
crossref_primary_10_1016_j_ast_2025_110121
crossref_primary_10_3390_aerospace12070618
crossref_primary_10_1016_j_cja_2024_08_020
crossref_primary_10_1177_09544100251360040
crossref_primary_10_1016_j_ast_2024_109768
Cites_doi 10.2514/1.58099
10.2514/1.14956
10.2514/1.G004513
10.2514/1.60356
10.1016/j.ifacol.2016.03.119
10.1109/TAES.2020.2976084
10.2514/1.G005250
10.1016/j.ast.2020.106134
10.1016/j.ast.2015.03.016
10.1016/j.ast.2021.106529
10.1109/TAES.2016.140861
10.1109/TAES.2018.2890375
10.1016/j.ast.2022.107552
10.1007/s10107-002-0349-3
10.1017/S0962492904000248
10.2514/1.50821
10.1016/j.ast.2021.106817
10.1016/j.ast.2021.107037
10.1016/j.ast.2016.12.022
10.1109/TAES.2016.150741
10.2514/1.G003359
10.2514/3.25376
10.1109/TAES.2017.2669598
10.2514/1.G003424
10.1016/j.cja.2021.05.021
10.2514/1.60075
10.1016/j.ast.2020.105841
10.2514/1.G000038
10.1016/j.ast.2018.03.038
ContentType Journal Article
Copyright 2023 Elsevier Masson SAS
Copyright_xml – notice: 2023 Elsevier Masson SAS
DBID AAYXX
CITATION
DOI 10.1016/j.ast.2023.108137
DatabaseName CrossRef
DatabaseTitle CrossRef
DatabaseTitleList
DeliveryMethod fulltext_linktorsrc
Discipline Engineering
EISSN 1626-3219
ExternalDocumentID 10_1016_j_ast_2023_108137
S1270963823000342
GroupedDBID --K
--M
.~1
0R~
1B1
1~.
1~5
23M
4.4
457
4G.
5GY
5VS
7-5
71M
8P~
AACTN
AAEDT
AAEDW
AAIAV
AAIKJ
AAKOC
AALRI
AAOAW
AAQFI
AAXUO
ABJNI
ABMAC
ABXDB
ABYKQ
ACDAQ
ACGFS
ACNNM
ACRLP
ADBBV
ADEZE
ADTZH
AEBSH
AECPX
AEKER
AENEX
AFKWA
AFTJW
AGHFR
AGUBO
AGYEJ
AHJVU
AHPGS
AI.
AIEXJ
AIKHN
AITUG
AJBFU
AJOXV
ALMA_UNASSIGNED_HOLDINGS
AMFUW
AMRAJ
ASPBG
AVWKF
AXJTR
AZFZN
BJAXD
BKOJK
BLXMC
CS3
EBS
EFJIC
EFLBG
EJD
EO8
EO9
EP2
EP3
FDB
FEDTE
FGOYB
FIRID
FNPLU
FYGXN
G-Q
GBLVA
HVGLF
HZ~
IHE
J1W
JJJVA
KOM
M41
MO0
N9A
O-L
O9-
OAUVE
OZT
P-8
P-9
P2P
PC.
Q38
R2-
RIG
ROL
RPZ
SDF
SDG
SDP
SES
SEW
SPC
SPCBC
SST
SSZ
T5K
T9H
VH1
XPP
ZMT
~G-
9DU
AATTM
AAXKI
AAYWO
AAYXX
ACLOT
ACVFH
ADCNI
AEIPS
AEUPX
AFJKZ
AFPUW
AIGII
AIIUN
AKBMS
AKRWK
AKYEP
ANKPU
APXCP
CITATION
EFKBS
~HD
ID FETCH-LOGICAL-c227t-b9f3299c38d42ea87329babcfd53d601a87d12fcc89dcf13d7a65542624ed1f93
ISICitedReferencesCount 12
ISICitedReferencesURI http://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=Summon&SrcAuth=ProQuest&DestLinkType=CitingArticles&DestApp=WOS_CPL&KeyUT=000945689700001&url=https%3A%2F%2Fcvtisr.summon.serialssolutions.com%2F%23%21%2Fsearch%3Fho%3Df%26include.ft.matches%3Dt%26l%3Dnull%26q%3D
ISSN 1270-9638
IngestDate Tue Nov 18 22:23:44 EST 2025
Sat Nov 29 07:04:59 EST 2025
Fri Feb 23 02:39:04 EST 2024
IsPeerReviewed true
IsScholarly true
Keywords Pseudospectral discretization
Model Predictive Static Programming (MPSP)
Midcourse guidance
Trajectory optimization
Active-set
Language English
LinkModel OpenURL
MergedId FETCHMERGED-LOGICAL-c227t-b9f3299c38d42ea87329babcfd53d601a87d12fcc89dcf13d7a65542624ed1f93
ORCID 0000-0002-8388-7588
0000-0003-1667-212X
0000-0002-2282-6001
0000-0001-7056-5902
ParticipantIDs crossref_primary_10_1016_j_ast_2023_108137
crossref_citationtrail_10_1016_j_ast_2023_108137
elsevier_sciencedirect_doi_10_1016_j_ast_2023_108137
PublicationCentury 2000
PublicationDate March 2023
2023-03-00
PublicationDateYYYYMMDD 2023-03-01
PublicationDate_xml – month: 03
  year: 2023
  text: March 2023
PublicationDecade 2020
PublicationTitle Aerospace science and technology
PublicationYear 2023
Publisher Elsevier Masson SAS
Publisher_xml – name: Elsevier Masson SAS
References Duvvuru, Maity, Umakant (br0260) 2022
Hough (br0040) 2018; 41
Dwivedi, Bhale, Bhattacharyya, Padhi (br0120) 2013
T.H. Phillips, A common aero vehicle (cav) model, description, and employment guide.
Ann, Lee, Kim, Ahn (br0200) 2020; 56
He, Yan (br0010) 2018; 41
Indig, Ben-Asher, Farber (br0130) 2013; 37
Imado, Kuroda, Miwa (br0090) 1990; 13
Dwivedi, Bhale, Bhattacharyya, Padhi (br0180) 2014; 37
Kumar, Dwivedi, Bhattacharyya, Padhi (br0170) 2017; 53
Zhang, Zhou (br0150) 2022; 35
P. Kumar, P. Dwivedi, A. Bhattacharya, Integrated guidance and control against high speed targets with desired aspect angle, in: Proc. AIAA Guid., Navig., Control Conf., pp. 2006–6783.
Majumder, Basha, Tiwari, Prasad, Sarkar (br0100) 2016; 49
Liu, Shen, Lu (br0320) 2016; 52
Dwivedi, Bhattacharya, Padhi (br0060) 2011; 34
Hough (br0050) 2019; 43
Dwivedi, Bhale, Bhattacharyya, Padhi (br0190) 2016; 52
Yan, He (br0270) 2020; 101
Li, He, Wang, Shin, Tsourdos (br0140) 2020; 44
Wan, Chang, Li, Yan (br0230) 2019; 2019
Annam, Ratnoo, Ghose (br0350) 2021
Yang, Jing, Gao (br0210) 2021; 118
Li, Zhang, Tang (br0020) 2015; 43
Pashupathy, Maity, Hong, Holzapfel (br0250) 2021; 116
Jorge, Stephen (br0290) 2006
Maity, Oza, Padhi (br0310) 2014; 37
Gould, Orban, Toint (br0300) 2005; 14
Andersen, Roos, Terlaky (br0280) 2003; 95
Zhu, He, Tang, Bao (br0030) 2018; 78
Guo, Hawkins, Wie (br0160) 2013; 36
Zarchan (br0330) 2012
Cheng, Yan, Tang, Wu, Li (br0360) 2021; 111
Zhou, Yan, Tang (br0220) 2020; 106
Ohlmeyer, Phillips (br0110) 2006; 29
Hong, Maity, Holzapfel, Tang (br0240) 2019; 55
Zhou, Lei, Zhang (br0070) 2017; 63
Dwivedi (10.1016/j.ast.2023.108137_br0190) 2016; 52
Imado (10.1016/j.ast.2023.108137_br0090) 1990; 13
Guo (10.1016/j.ast.2023.108137_br0160) 2013; 36
Zhou (10.1016/j.ast.2023.108137_br0220) 2020; 106
Cheng (10.1016/j.ast.2023.108137_br0360) 2021; 111
Hong (10.1016/j.ast.2023.108137_br0240) 2019; 55
Hough (10.1016/j.ast.2023.108137_br0050) 2019; 43
Zhou (10.1016/j.ast.2023.108137_br0070) 2017; 63
Dwivedi (10.1016/j.ast.2023.108137_br0060) 2011; 34
Dwivedi (10.1016/j.ast.2023.108137_br0120) 2013
Wan (10.1016/j.ast.2023.108137_br0230) 2019; 2019
Ann (10.1016/j.ast.2023.108137_br0200) 2020; 56
10.1016/j.ast.2023.108137_br0080
10.1016/j.ast.2023.108137_br0340
Zhang (10.1016/j.ast.2023.108137_br0150) 2022; 35
He (10.1016/j.ast.2023.108137_br0010) 2018; 41
Liu (10.1016/j.ast.2023.108137_br0320) 2016; 52
Hough (10.1016/j.ast.2023.108137_br0040) 2018; 41
Jorge (10.1016/j.ast.2023.108137_br0290) 2006
Li (10.1016/j.ast.2023.108137_br0020) 2015; 43
Yang (10.1016/j.ast.2023.108137_br0210) 2021; 118
Annam (10.1016/j.ast.2023.108137_br0350) 2021
Pashupathy (10.1016/j.ast.2023.108137_br0250) 2021; 116
Maity (10.1016/j.ast.2023.108137_br0310) 2014; 37
Dwivedi (10.1016/j.ast.2023.108137_br0180) 2014; 37
Ohlmeyer (10.1016/j.ast.2023.108137_br0110) 2006; 29
Indig (10.1016/j.ast.2023.108137_br0130) 2013; 37
Gould (10.1016/j.ast.2023.108137_br0300) 2005; 14
Zhu (10.1016/j.ast.2023.108137_br0030) 2018; 78
Duvvuru (10.1016/j.ast.2023.108137_br0260) 2022
Yan (10.1016/j.ast.2023.108137_br0270) 2020; 101
Majumder (10.1016/j.ast.2023.108137_br0100) 2016; 49
Li (10.1016/j.ast.2023.108137_br0140) 2020; 44
Kumar (10.1016/j.ast.2023.108137_br0170) 2017; 53
Zarchan (10.1016/j.ast.2023.108137_br0330) 2012
Andersen (10.1016/j.ast.2023.108137_br0280) 2003; 95
References_xml – volume: 95
  start-page: 249
  year: 2003
  end-page: 277
  ident: br0280
  article-title: On implementing a primal-dual interior-point method for conic quadratic optimization
  publication-title: Math. Program.
– volume: 44
  start-page: 172
  year: 2020
  end-page: 180
  ident: br0140
  article-title: Near-optimal midcourse guidance for velocity maximization with constrained arrival angle
  publication-title: J. Guid. Control Dyn.
– volume: 13
  start-page: 603
  year: 1990
  end-page: 608
  ident: br0090
  article-title: Optimal midcourse guidance for medium-range air-to-air missiles
  publication-title: J. Guid. Control Dyn.
– volume: 29
  start-page: 261
  year: 2006
  end-page: 268
  ident: br0110
  article-title: Generalized vector explicit guidance
  publication-title: J. Guid. Control Dyn.
– volume: 41
  start-page: 1591
  year: 2018
  end-page: 1601
  ident: br0010
  article-title: Adaptive terminal guidance law for spiral-diving maneuver based on virtual sliding targets
  publication-title: J. Guid. Control Dyn.
– year: 2013
  ident: br0120
  article-title: Lead Angle Constrained Optimal Midcourse Guidance, Guidance, Navigation, and Control and Co-located Conferences
– volume: 37
  start-page: 243
  year: 2014
  end-page: 264
  ident: br0180
  article-title: Generalized state estimation and model predictive guidance for spiraling and ballistic targets
  publication-title: J. Guid. Control Dyn.
– volume: 56
  start-page: 3655
  year: 2020
  end-page: 3673
  ident: br0200
  article-title: Midcourse guidance for exoatmospheric interception using response surface based trajectory shaping
  publication-title: IEEE Trans. Aerosp. Electron. Syst.
– volume: 118
  year: 2021
  ident: br0210
  article-title: Online midcourse guidance method for boost phase interception via adaptive convex programming
  publication-title: Aerosp. Sci. Technol.
– year: 2006
  ident: br0290
– year: 2012
  ident: br0330
  article-title: Tactical and Strategic Missile Guidance
– start-page: 1
  year: 2021
  end-page: 15
  ident: br0350
  article-title: Singular-perturbation-based guidance of pulse motor interceptors with look angle constraints
  publication-title: J. Guid. Control Dyn.
– volume: 111
  year: 2021
  ident: br0360
  article-title: An adaptive non-zero mean damping model for trajectory tracking of hypersonic glide vehicles
  publication-title: Aerosp. Sci. Technol.
– volume: 41
  start-page: 1463
  year: 2018
  end-page: 1475
  ident: br0040
  article-title: Acceleration characterization for reentry orbit determination with unmodeled maneuvers
  publication-title: J. Guid. Control Dyn.
– volume: 35
  start-page: 320
  year: 2022
  end-page: 331
  ident: br0150
  article-title: Optimal predictive sliding-mode guidance law for intercepting near-space hypersonic maneuvering target
  publication-title: Chin. J. Aeronaut.
– volume: 34
  start-page: 860
  year: 2011
  end-page: 877
  ident: br0060
  article-title: Suboptimal midcourse guidance of interceptors for high-speed targets with alignment angle constraint
  publication-title: J. Guid. Control Dyn.
– volume: 2019
  year: 2019
  ident: br0230
  article-title: Suboptimal midcourse guidance with terminal-angle constraint for hypersonic target interception
  publication-title: Int. J. Aerosp. Eng.
– volume: 52
  start-page: 2111
  year: 2016
  end-page: 2122
  ident: br0190
  article-title: Generalized estimation and predictive guidance for evasive targets
  publication-title: IEEE Trans. Aerosp. Electron. Syst.
– volume: 52
  start-page: 1881
  year: 2016
  end-page: 1892
  ident: br0320
  article-title: Exact convex relaxation for optimal flight of aerodynamically controlled missiles
  publication-title: IEEE Trans. Aerosp. Electron. Syst.
– volume: 106
  year: 2020
  ident: br0220
  article-title: Generalized quasi-spectral model predictive static programming method using Gaussian quadrature collocation
  publication-title: Aerosp. Sci. Technol.
– reference: P. Kumar, P. Dwivedi, A. Bhattacharya, Integrated guidance and control against high speed targets with desired aspect angle, in: Proc. AIAA Guid., Navig., Control Conf., pp. 2006–6783.
– volume: 43
  start-page: 321
  year: 2015
  end-page: 328
  ident: br0020
  article-title: Maneuver characteristics analysis for hypersonic glide vehicles
  publication-title: Aerosp. Sci. Technol.
– volume: 101
  year: 2020
  ident: br0270
  article-title: Unpowered approach and landing trajectory planning using second-order cone programming
  publication-title: Aerosp. Sci. Technol.
– reference: T.H. Phillips, A common aero vehicle (cav) model, description, and employment guide.
– volume: 116
  year: 2021
  ident: br0250
  article-title: Unspecified final-time nonlinear suboptimal guidance of aerobatic aircraft in air race
  publication-title: Aerosp. Sci. Technol.
– volume: 63
  start-page: 266
  year: 2017
  end-page: 277
  ident: br0070
  article-title: Online optimal midcourse trajectory modification algorithm for hypersonic vehicle interceptions
  publication-title: Aerosp. Sci. Technol.
– volume: 53
  start-page: 1250
  year: 2017
  end-page: 1260
  ident: br0170
  article-title: Terminal-lead-angle-constrained generalized explicit guidance
  publication-title: IEEE Trans. Aerosp. Electron. Syst.
– volume: 36
  start-page: 810
  year: 2013
  end-page: 820
  ident: br0160
  article-title: Applications of generalized zero-effort-miss/zero-effort-velocity feedback guidance algorithm
  publication-title: J. Guid. Control Dyn.
– volume: 14
  start-page: 299
  year: 2005
  end-page: 361
  ident: br0300
  article-title: Numerical methods for large-scale nonlinear optimization
  publication-title: Acta Numer.
– volume: 37
  start-page: 1897
  year: 2014
  end-page: 1913
  ident: br0310
  article-title: Generalized model predictive static programming and angle-constrained guidance of air-to-ground missiles
  publication-title: J. Guid. Control Dyn.
– volume: 43
  start-page: 422
  year: 2019
  end-page: 437
  ident: br0050
  article-title: Precise reentry maneuver estimation using radar trilateration
  publication-title: J. Guid. Control Dyn.
– volume: 49
  start-page: 591
  year: 2016
  end-page: 596
  ident: br0100
  article-title: Practical aspects of optimal midcourse guidance for air-to-air engagement
  publication-title: IFAC-PapersOnLine
– volume: 78
  start-page: 62
  year: 2018
  end-page: 70
  ident: br0030
  article-title: Pendulum maneuvering strategy for hypersonic glide vehicles
  publication-title: Aerosp. Sci. Technol.
– volume: 37
  start-page: 214
  year: 2013
  end-page: 223
  ident: br0130
  article-title: Near-optimal spatial midcourse guidance law with an angular constraint
  publication-title: J. Guid. Control Dyn.
– year: 2022
  ident: br0260
  article-title: Three-dimensional field of view and impact angle constrained guidance with terminal speed maximization
  publication-title: Aerosp. Sci. Technol.
– volume: 55
  start-page: 2487
  year: 2019
  end-page: 2500
  ident: br0240
  article-title: Model predictive convex programming for constrained vehicle guidance
  publication-title: IEEE Trans. Aerosp. Electron. Syst.
– volume: 36
  start-page: 810
  issue: 3
  year: 2013
  ident: 10.1016/j.ast.2023.108137_br0160
  article-title: Applications of generalized zero-effort-miss/zero-effort-velocity feedback guidance algorithm
  publication-title: J. Guid. Control Dyn.
  doi: 10.2514/1.58099
– volume: 29
  start-page: 261
  issue: 2
  year: 2006
  ident: 10.1016/j.ast.2023.108137_br0110
  article-title: Generalized vector explicit guidance
  publication-title: J. Guid. Control Dyn.
  doi: 10.2514/1.14956
– volume: 43
  start-page: 422
  issue: 3
  year: 2019
  ident: 10.1016/j.ast.2023.108137_br0050
  article-title: Precise reentry maneuver estimation using radar trilateration
  publication-title: J. Guid. Control Dyn.
  doi: 10.2514/1.G004513
– volume: 37
  start-page: 214
  issue: 1
  year: 2013
  ident: 10.1016/j.ast.2023.108137_br0130
  article-title: Near-optimal spatial midcourse guidance law with an angular constraint
  publication-title: J. Guid. Control Dyn.
  doi: 10.2514/1.60356
– volume: 49
  start-page: 591
  issue: 1
  year: 2016
  ident: 10.1016/j.ast.2023.108137_br0100
  article-title: Practical aspects of optimal midcourse guidance for air-to-air engagement
  publication-title: IFAC-PapersOnLine
  doi: 10.1016/j.ifacol.2016.03.119
– volume: 56
  start-page: 3655
  issue: 5
  year: 2020
  ident: 10.1016/j.ast.2023.108137_br0200
  article-title: Midcourse guidance for exoatmospheric interception using response surface based trajectory shaping
  publication-title: IEEE Trans. Aerosp. Electron. Syst.
  doi: 10.1109/TAES.2020.2976084
– volume: 44
  start-page: 172
  issue: 1
  year: 2020
  ident: 10.1016/j.ast.2023.108137_br0140
  article-title: Near-optimal midcourse guidance for velocity maximization with constrained arrival angle
  publication-title: J. Guid. Control Dyn.
  doi: 10.2514/1.G005250
– volume: 106
  year: 2020
  ident: 10.1016/j.ast.2023.108137_br0220
  article-title: Generalized quasi-spectral model predictive static programming method using Gaussian quadrature collocation
  publication-title: Aerosp. Sci. Technol.
  doi: 10.1016/j.ast.2020.106134
– volume: 43
  start-page: 321
  year: 2015
  ident: 10.1016/j.ast.2023.108137_br0020
  article-title: Maneuver characteristics analysis for hypersonic glide vehicles
  publication-title: Aerosp. Sci. Technol.
  doi: 10.1016/j.ast.2015.03.016
– year: 2012
  ident: 10.1016/j.ast.2023.108137_br0330
– ident: 10.1016/j.ast.2023.108137_br0080
– year: 2006
  ident: 10.1016/j.ast.2023.108137_br0290
– ident: 10.1016/j.ast.2023.108137_br0340
– volume: 111
  year: 2021
  ident: 10.1016/j.ast.2023.108137_br0360
  article-title: An adaptive non-zero mean damping model for trajectory tracking of hypersonic glide vehicles
  publication-title: Aerosp. Sci. Technol.
  doi: 10.1016/j.ast.2021.106529
– volume: 52
  start-page: 2111
  issue: 5
  year: 2016
  ident: 10.1016/j.ast.2023.108137_br0190
  article-title: Generalized estimation and predictive guidance for evasive targets
  publication-title: IEEE Trans. Aerosp. Electron. Syst.
  doi: 10.1109/TAES.2016.140861
– volume: 55
  start-page: 2487
  issue: 5
  year: 2019
  ident: 10.1016/j.ast.2023.108137_br0240
  article-title: Model predictive convex programming for constrained vehicle guidance
  publication-title: IEEE Trans. Aerosp. Electron. Syst.
  doi: 10.1109/TAES.2018.2890375
– start-page: 1
  year: 2021
  ident: 10.1016/j.ast.2023.108137_br0350
  article-title: Singular-perturbation-based guidance of pulse motor interceptors with look angle constraints
  publication-title: J. Guid. Control Dyn.
– year: 2022
  ident: 10.1016/j.ast.2023.108137_br0260
  article-title: Three-dimensional field of view and impact angle constrained guidance with terminal speed maximization
  publication-title: Aerosp. Sci. Technol.
  doi: 10.1016/j.ast.2022.107552
– volume: 2019
  year: 2019
  ident: 10.1016/j.ast.2023.108137_br0230
  article-title: Suboptimal midcourse guidance with terminal-angle constraint for hypersonic target interception
  publication-title: Int. J. Aerosp. Eng.
– volume: 95
  start-page: 249
  issue: 2
  year: 2003
  ident: 10.1016/j.ast.2023.108137_br0280
  article-title: On implementing a primal-dual interior-point method for conic quadratic optimization
  publication-title: Math. Program.
  doi: 10.1007/s10107-002-0349-3
– volume: 14
  start-page: 299
  year: 2005
  ident: 10.1016/j.ast.2023.108137_br0300
  article-title: Numerical methods for large-scale nonlinear optimization
  publication-title: Acta Numer.
  doi: 10.1017/S0962492904000248
– volume: 34
  start-page: 860
  issue: 3
  year: 2011
  ident: 10.1016/j.ast.2023.108137_br0060
  article-title: Suboptimal midcourse guidance of interceptors for high-speed targets with alignment angle constraint
  publication-title: J. Guid. Control Dyn.
  doi: 10.2514/1.50821
– volume: 116
  year: 2021
  ident: 10.1016/j.ast.2023.108137_br0250
  article-title: Unspecified final-time nonlinear suboptimal guidance of aerobatic aircraft in air race
  publication-title: Aerosp. Sci. Technol.
  doi: 10.1016/j.ast.2021.106817
– volume: 118
  year: 2021
  ident: 10.1016/j.ast.2023.108137_br0210
  article-title: Online midcourse guidance method for boost phase interception via adaptive convex programming
  publication-title: Aerosp. Sci. Technol.
  doi: 10.1016/j.ast.2021.107037
– volume: 63
  start-page: 266
  issue: 4
  year: 2017
  ident: 10.1016/j.ast.2023.108137_br0070
  article-title: Online optimal midcourse trajectory modification algorithm for hypersonic vehicle interceptions
  publication-title: Aerosp. Sci. Technol.
  doi: 10.1016/j.ast.2016.12.022
– volume: 52
  start-page: 1881
  issue: 4
  year: 2016
  ident: 10.1016/j.ast.2023.108137_br0320
  article-title: Exact convex relaxation for optimal flight of aerodynamically controlled missiles
  publication-title: IEEE Trans. Aerosp. Electron. Syst.
  doi: 10.1109/TAES.2016.150741
– volume: 41
  start-page: 1463
  issue: 7
  year: 2018
  ident: 10.1016/j.ast.2023.108137_br0040
  article-title: Acceleration characterization for reentry orbit determination with unmodeled maneuvers
  publication-title: J. Guid. Control Dyn.
  doi: 10.2514/1.G003359
– year: 2013
  ident: 10.1016/j.ast.2023.108137_br0120
– volume: 13
  start-page: 603
  issue: 4
  year: 1990
  ident: 10.1016/j.ast.2023.108137_br0090
  article-title: Optimal midcourse guidance for medium-range air-to-air missiles
  publication-title: J. Guid. Control Dyn.
  doi: 10.2514/3.25376
– volume: 53
  start-page: 1250
  issue: 3
  year: 2017
  ident: 10.1016/j.ast.2023.108137_br0170
  article-title: Terminal-lead-angle-constrained generalized explicit guidance
  publication-title: IEEE Trans. Aerosp. Electron. Syst.
  doi: 10.1109/TAES.2017.2669598
– volume: 41
  start-page: 1591
  issue: 7
  year: 2018
  ident: 10.1016/j.ast.2023.108137_br0010
  article-title: Adaptive terminal guidance law for spiral-diving maneuver based on virtual sliding targets
  publication-title: J. Guid. Control Dyn.
  doi: 10.2514/1.G003424
– volume: 35
  start-page: 320
  issue: 4
  year: 2022
  ident: 10.1016/j.ast.2023.108137_br0150
  article-title: Optimal predictive sliding-mode guidance law for intercepting near-space hypersonic maneuvering target
  publication-title: Chin. J. Aeronaut.
  doi: 10.1016/j.cja.2021.05.021
– volume: 37
  start-page: 243
  issue: 1
  year: 2014
  ident: 10.1016/j.ast.2023.108137_br0180
  article-title: Generalized state estimation and model predictive guidance for spiraling and ballistic targets
  publication-title: J. Guid. Control Dyn.
  doi: 10.2514/1.60075
– volume: 101
  year: 2020
  ident: 10.1016/j.ast.2023.108137_br0270
  article-title: Unpowered approach and landing trajectory planning using second-order cone programming
  publication-title: Aerosp. Sci. Technol.
  doi: 10.1016/j.ast.2020.105841
– volume: 37
  start-page: 1897
  issue: 6
  year: 2014
  ident: 10.1016/j.ast.2023.108137_br0310
  article-title: Generalized model predictive static programming and angle-constrained guidance of air-to-ground missiles
  publication-title: J. Guid. Control Dyn.
  doi: 10.2514/1.G000038
– volume: 78
  start-page: 62
  year: 2018
  ident: 10.1016/j.ast.2023.108137_br0030
  article-title: Pendulum maneuvering strategy for hypersonic glide vehicles
  publication-title: Aerosp. Sci. Technol.
  doi: 10.1016/j.ast.2018.03.038
SSID ssj0002942
Score 2.3959575
Snippet This paper focuses on the midcourse guidance law for the interceptor to engage the hypersonic gliding vehicles (HGVs). Firstly, an active-set pseudospectral...
SourceID crossref
elsevier
SourceType Enrichment Source
Index Database
Publisher
StartPage 108137
SubjectTerms Active-set
Midcourse guidance
Model Predictive Static Programming (MPSP)
Pseudospectral discretization
Trajectory optimization
Title Active-set pseudospectral model predictive static programming for midcourse guidance
URI https://dx.doi.org/10.1016/j.ast.2023.108137
Volume 134
WOSCitedRecordID wos000945689700001&url=https%3A%2F%2Fcvtisr.summon.serialssolutions.com%2F%23%21%2Fsearch%3Fho%3Df%26include.ft.matches%3Dt%26l%3Dnull%26q%3D
hasFullText 1
inHoldings 1
isFullTextHit
isPrint
journalDatabaseRights – providerCode: PRVESC
  databaseName: Elsevier SD Freedom Collection Journals 2021
  customDbUrl:
  eissn: 1626-3219
  dateEnd: 99991231
  omitProxy: false
  ssIdentifier: ssj0002942
  issn: 1270-9638
  databaseCode: AIEXJ
  dateStart: 19970101
  isFulltext: true
  titleUrlDefault: https://www.sciencedirect.com
  providerName: Elsevier
link http://cvtisr.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwtV3di9QwEA9654M-iJ94fpEHn1wibdptm8dFTlTwEG6FxZeSZFLt4bXrdVfuz3fy1a53Kir4UrYhaZbMr5OZ6S8zhDxrqqRS81yzFAp0ULRQTFa8YaBSEFLjDqbBFZsoj46q1Uq8D7SiwZUTKLuuOj8X6_8qamxDYdujs38h7vGh2IC_Ueh4RbHj9Y8Ev3AajA1mM1sPZgu9O0xpz-G7qjc2KwC0ro-NI9h8rYGjdRpJlact6N6SO2afti2MsIi5ag1urOhpm1k8EuRImJdC9B8_91sXhu3D5ugiri4OYNpR2fj466qV6B5P_SzX1pnVsvsaUoOHyATPJmqWD5fFIzPv0A2wym9xvKNoeZkw-_L7fci3oXPFsqhCo3b2sc5Lmt4HHU5eyMEyYnlmyZKpzx9zIYH2sZ3LToXelst4eJXs83IuUAfuL94crt6OOzcXrtjS-N_iV3DHB7ww0c_tmB3bZHmL3AxOBV14MNwmV0x3h9zYSTV5lywnWNAfYUEdLOgEC-phQXdgQREWdIQFjbC4Rz68Oly-fM1CRQ2mOS83TIkmQ_tDZxXk3MiqxDsllW5gngG65tgCKW-0rgToJs2glAXam7zguYG0Edl9stf1nXlAqASRawWF1Ankc64UpKlQ-LIXSiuTJwckietT65Bu3lY9-VJHXuFJjUta2yWt_ZIekOfjkLXPtfK7znlc9DrA3RuBNSLk18Me_tuwR-T6hPDHZG9ztjVPyDX9bdMOZ08Djr4DqiqRgQ
linkProvider Elsevier
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=Active-set+pseudospectral+model+predictive+static+programming+for+midcourse+guidance&rft.jtitle=Aerospace+science+and+technology&rft.au=Zhou%2C+Cong&rft.au=He%2C+Lei&rft.au=Yan%2C+Xiaodong&rft.au=Meng%2C+Fanqin&rft.date=2023-03-01&rft.pub=Elsevier+Masson+SAS&rft.issn=1270-9638&rft.eissn=1626-3219&rft.volume=134&rft_id=info:doi/10.1016%2Fj.ast.2023.108137&rft.externalDocID=S1270963823000342
thumbnail_l http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/lc.gif&issn=1270-9638&client=summon
thumbnail_m http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/mc.gif&issn=1270-9638&client=summon
thumbnail_s http://covers-cdn.summon.serialssolutions.com/index.aspx?isbn=/sc.gif&issn=1270-9638&client=summon