Noniterative feedback midcourse guidance for exo-atmospheric interception of ballistic targets using virtual impact point steering
This paper proposes a noniterative feedback midcourse guidance algorithm for intercepting a ballistic target. The virtual impact point (VIP) concept, which is the intersection point between the defense missile trajectory and the sphere defined by the hit altitude, is introduced. Then the motion of t...
Uloženo v:
| Vydáno v: | Aerospace science and technology Ročník 119; s. 107159 |
|---|---|
| Hlavní autoři: | , |
| Médium: | Journal Article |
| Jazyk: | angličtina |
| Vydáno: |
Elsevier Masson SAS
01.12.2021
|
| Témata: | |
| ISSN: | 1270-9638, 1626-3219 |
| On-line přístup: | Získat plný text |
| Tagy: |
Přidat tag
Žádné tagy, Buďte první, kdo vytvoří štítek k tomuto záznamu!
|
| Abstract | This paper proposes a noniterative feedback midcourse guidance algorithm for intercepting a ballistic target. The virtual impact point (VIP) concept, which is the intersection point between the defense missile trajectory and the sphere defined by the hit altitude, is introduced. Then the motion of the virtual impact point caused by the external acceleration applied to the missile is derived. The proposed guidance algorithm generates the acceleration command that moves the VIP to the PIP along the shortest path without any iterative procedure and has high potential as an onboard midcourse guidance algorithm. The validity of the proposed guidance algorithm has been demonstrated through the case study. |
|---|---|
| AbstractList | This paper proposes a noniterative feedback midcourse guidance algorithm for intercepting a ballistic target. The virtual impact point (VIP) concept, which is the intersection point between the defense missile trajectory and the sphere defined by the hit altitude, is introduced. Then the motion of the virtual impact point caused by the external acceleration applied to the missile is derived. The proposed guidance algorithm generates the acceleration command that moves the VIP to the PIP along the shortest path without any iterative procedure and has high potential as an onboard midcourse guidance algorithm. The validity of the proposed guidance algorithm has been demonstrated through the case study. |
| ArticleNumber | 107159 |
| Author | Jo, Byeong-Un Ahn, Jaemyung |
| Author_xml | – sequence: 1 givenname: Byeong-Un orcidid: 0000-0003-0841-8607 surname: Jo fullname: Jo, Byeong-Un – sequence: 2 givenname: Jaemyung orcidid: 0000-0003-4971-5130 surname: Ahn fullname: Ahn, Jaemyung email: jaemyung.ahn@kaist.ac.kr |
| BookMark | eNp9kL9OAzEMhyMEEqXwAGx5gSvJHb00YkKIfxKCpXuUc5zicr2ckrSClScnVZkYmGzrp8-yvzN2PIQBGbuUYiaFbK_WM5vyrBa1LLOSc33EJrKt26qppT4ufa1EpdtmccrOUloLIWp9XU_Y92sYKGO0mXbIPaLrLHzwDTkI25iQr7bk7AAlC5HjZ6hs3oQ0vmMk4DQUFHDMFAYePO9s31PKJck2rjAnvk00rPiOYt7antNmtJD5GArIU8ayZFidsxNv-4QXv3XKlg_3y7un6uXt8fnu9qWCWqtcudZKBAFCaeU9Ou2wXOth0XVzwIVohWxAo9WdktIq55VTvp3LOSI0DTZTJg9rIYaUInozRtrY-GWkMHuHZm2KQ7N3aA4OC6P-MEDZ7r_N0VL_L3lzILF8tCOMJgFh8egoImTjAv1D_wCfSZP5 |
| CitedBy_id | crossref_primary_10_2514_1_G007760 crossref_primary_10_1016_j_ast_2022_108031 crossref_primary_10_1016_j_conengprac_2025_106242 crossref_primary_10_1016_j_ast_2025_110296 crossref_primary_10_1016_j_asr_2025_08_004 |
| Cites_doi | 10.2514/3.20181 10.1016/j.ast.2019.105633 10.1109/TAES.2020.2976084 10.2514/1.G005059 10.1145/1731022.1731032 10.1016/j.ast.2019.01.012 10.1016/j.asoc.2014.02.015 10.2514/1.50821 10.2514/1.59625 10.1155/2019/8502870 10.2514/1.60356 10.1109/6.619381 10.2514/3.25375 10.2514/1.61681 10.2514/3.20081 10.1016/j.ast.2018.02.024 10.2514/3.21586 10.2514/1.G004703 10.2514/3.21410 10.2514/1.36961 10.1016/j.ast.2020.105746 10.2514/1.1679 10.2514/1.44430 10.2514/1.56395 |
| ContentType | Journal Article |
| Copyright | 2021 Elsevier Masson SAS |
| Copyright_xml | – notice: 2021 Elsevier Masson SAS |
| DBID | AAYXX CITATION |
| DOI | 10.1016/j.ast.2021.107159 |
| DatabaseName | CrossRef |
| DatabaseTitle | CrossRef |
| DatabaseTitleList | |
| DeliveryMethod | fulltext_linktorsrc |
| Discipline | Engineering |
| EISSN | 1626-3219 |
| ExternalDocumentID | 10_1016_j_ast_2021_107159 S1270963821006696 |
| 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-c297t-d6a1ec0c0797ffed9deeedfc8bb5ce806013c9ea9b711a7df7d7f6515eec33e3 |
| ISICitedReferencesCount | 10 |
| ISICitedReferencesURI | http://www.webofscience.com/api/gateway?GWVersion=2&SrcApp=Summon&SrcAuth=ProQuest&DestLinkType=CitingArticles&DestApp=WOS_CPL&KeyUT=000711641200004&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 | Sat Nov 29 07:00:53 EST 2025 Tue Nov 18 22:22:14 EST 2025 Fri Feb 23 02:41:04 EST 2024 |
| IsPeerReviewed | true |
| IsScholarly | true |
| Keywords | Instantaneous impact point Missile defense Midcourse guidance Exo-atmospheric interception Ballistic target |
| Language | English |
| LinkModel | OpenURL |
| MergedId | FETCHMERGED-LOGICAL-c297t-d6a1ec0c0797ffed9deeedfc8bb5ce806013c9ea9b711a7df7d7f6515eec33e3 |
| ORCID | 0000-0003-4971-5130 0000-0003-0841-8607 |
| ParticipantIDs | crossref_primary_10_1016_j_ast_2021_107159 crossref_citationtrail_10_1016_j_ast_2021_107159 elsevier_sciencedirect_doi_10_1016_j_ast_2021_107159 |
| PublicationCentury | 2000 |
| PublicationDate | December 2021 2021-12-00 |
| PublicationDateYYYYMMDD | 2021-12-01 |
| PublicationDate_xml | – month: 12 year: 2021 text: December 2021 |
| PublicationDecade | 2020 |
| PublicationTitle | Aerospace science and technology |
| PublicationYear | 2021 |
| Publisher | Elsevier Masson SAS |
| Publisher_xml | – name: Elsevier Masson SAS |
| References | Cheng, Gupta (br0040) 1986; 9 Zhao, Li, Yang, Li (br0260) 2019; 86 Menon, Briggs (br0050) 1990; 13 Zhang, Xu (br0220) 2020; 97 Ann, Lee, Kim, Ahn (br0130) 2020; 56 Zes (br0090) 1994 Zes (br0110) 1998 Singh, Padmanabhan, Agarwal (br0230) 2014; 19 Lin, Tsai (br0060) 1987; 10 Burns, Scherock (br0160) 2004; 27 Creagh, Meagh (br0280) 2010; 33 Gaudet, Furfaro, Linares (br0030) 2020; 99 Jo, Ahn (br0180) 2018; 76 Zarchan (br0150) 2007 Ahn, Seo (br0250) 2013; 36 Jo, Ahn, Roh (br0190) 2020; 43 Rao, Benson, Darby, Patterson, Francolin, Sanders, Huntington (br0240) 2010; 37 Sullins (br0020) 2001; 22 Indig, Ben-Asher, Farber (br0070) 2014; 37 Na, Lee, Lee (br0140) 2020; 43 Newman (br0100) 1996; 19 Ahn, Roh (br0210) 2014; 37 Du, Chen, Yang, Zhou (br0170) 2019; 2019 Dwivedi, Bhattacharya, Padhi (br0080) 2011; 34 Lewis, Postol (br0010) 1997; 34 Massoumnia (br0120) 1995; 18 Shtessel, Tournes (br0270) 2009; 32 Ahn, Roh (br0200) 2012; 35 Rao (10.1016/j.ast.2021.107159_br0240) 2010; 37 Ahn (10.1016/j.ast.2021.107159_br0210) 2014; 37 Singh (10.1016/j.ast.2021.107159_br0230) 2014; 19 Sullins (10.1016/j.ast.2021.107159_br0020) 2001; 22 Massoumnia (10.1016/j.ast.2021.107159_br0120) 1995; 18 Ahn (10.1016/j.ast.2021.107159_br0250) 2013; 36 Burns (10.1016/j.ast.2021.107159_br0160) 2004; 27 Du (10.1016/j.ast.2021.107159_br0170) 2019; 2019 Lewis (10.1016/j.ast.2021.107159_br0010) 1997; 34 Menon (10.1016/j.ast.2021.107159_br0050) 1990; 13 Jo (10.1016/j.ast.2021.107159_br0190) 2020; 43 Jo (10.1016/j.ast.2021.107159_br0180) 2018; 76 Creagh (10.1016/j.ast.2021.107159_br0280) 2010; 33 Cheng (10.1016/j.ast.2021.107159_br0040) 1986; 9 Zhao (10.1016/j.ast.2021.107159_br0260) 2019; 86 Na (10.1016/j.ast.2021.107159_br0140) 2020; 43 Shtessel (10.1016/j.ast.2021.107159_br0270) 2009; 32 Dwivedi (10.1016/j.ast.2021.107159_br0080) 2011; 34 Zes (10.1016/j.ast.2021.107159_br0090) 1994 Ann (10.1016/j.ast.2021.107159_br0130) 2020; 56 Zarchan (10.1016/j.ast.2021.107159_br0150) 2007 Ahn (10.1016/j.ast.2021.107159_br0200) 2012; 35 Gaudet (10.1016/j.ast.2021.107159_br0030) 2020; 99 Indig (10.1016/j.ast.2021.107159_br0070) 2014; 37 Zes (10.1016/j.ast.2021.107159_br0110) 1998 Lin (10.1016/j.ast.2021.107159_br0060) 1987; 10 Zhang (10.1016/j.ast.2021.107159_br0220) 2020; 97 Newman (10.1016/j.ast.2021.107159_br0100) 1996; 19 |
| References_xml | – volume: 36 start-page: 958 year: 2013 end-page: 966 ident: br0250 article-title: Instantaneous impact point prediction using the response surface meth-od publication-title: J. Guid. Control Dyn. – volume: 37 start-page: 1 year: 2010 end-page: 39 ident: br0240 article-title: Algorithm 902: GPOPS, a Matlab software for solving multiple-phase optimal control problems using the Gauss pseudospectral method publication-title: ACM Trans. Math. Softw. – volume: 34 start-page: 60 year: 1997 end-page: 68 ident: br0010 article-title: Future challenges to ballistic missile defense publication-title: IEEE Spectr. – volume: 43 start-page: 373 year: 2020 end-page: 382 ident: br0190 article-title: Instantaneous impact point guidance considering uncertainty in engine cutoff time publication-title: J. Guid. Control Dyn. – volume: 34 start-page: 860 year: 2011 end-page: 877 ident: br0080 article-title: Suboptimal midcourse guidance of interceptors for high-speed targets with alignment angle constraint publication-title: J. Guid. Control Dyn. – volume: 9 start-page: 103 year: 1986 end-page: 107 ident: br0040 article-title: Advanced midcourse guidance for air to air missiles publication-title: J. Guid. Control Dyn. – volume: 2019 start-page: 1 year: 2019 end-page: 17 ident: br0170 article-title: Optimal midcourse guidance algorithm for exoatmospheric interception using analytical gradients publication-title: Int. J. Aerosp. Eng. – volume: 32 start-page: 79 year: 2009 end-page: 94 ident: br0270 article-title: Integrated higher-order sliding mode guidance and autopilot for dual-control missiles publication-title: J. Guid. Control Dyn. – volume: 22 start-page: 260 year: 2001 end-page: 274 ident: br0020 article-title: Exo-atmospheric intercepts: bringing new challenges to standard missile publication-title: Johns Hopkins APL Tech. Dig. – volume: 19 start-page: 280 year: 2014 end-page: 289 ident: br0230 article-title: Dynamic classification of ballistic missiles using neural networks and hidden Markov models publication-title: Appl. Soft Comput. – volume: 99 year: 2020 ident: br0030 article-title: Reinforcement learning for angle-only intercept guidance of maneuvering targets publication-title: Aerosp. Sci. Technol. – volume: 76 start-page: 523 year: 2018 end-page: 529 ident: br0180 article-title: Near time-optimal feedback instantaneous impact point (IIP) guidance law for rocket publication-title: Aerosp. Sci. Technol. – volume: 97 year: 2020 ident: br0220 article-title: Autonomous ascent guidance with multiple terminal constraints for all-solid launch vehicles publication-title: Aerosp. Sci. Technol. – volume: 27 start-page: 989 year: 2004 end-page: 996 ident: br0160 article-title: Lambert guidance routine designed to match position and velocity of ballistic target publication-title: J. Guid. Control Dyn. – volume: 10 start-page: 61 year: 1987 end-page: 66 ident: br0060 article-title: Analytical solution of optimal trajectory-shaping guidance publication-title: J. Guid. Control Dyn. – volume: 37 start-page: 214 year: 2014 end-page: 223 ident: br0070 article-title: Near-optimal spatial midcourse guidance law with an angular constraint publication-title: J. Guid. Control Dyn. – volume: 86 start-page: 256 year: 2019 end-page: 267 ident: br0260 article-title: Output feedback continuous terminal sliding mode guidance law for missile-target interception with autopilot dynamics publication-title: Aerosp. Sci. Technol. – volume: 33 start-page: 915 year: 2010 end-page: 922 ident: br0280 article-title: Attitude guidance for spinning vehicles with independent pitch and yaw control publication-title: J. Guid. Control Dyn. – year: 1994 ident: br0090 article-title: Exo-atmospheric intercept using modified proportional guidance with gravity correction for coast phase publication-title: 32nd Aerospace Sciences Meeting and Exhibit – year: 1998 ident: br0110 article-title: Exo-atmospheric intercept with J2 correction publication-title: Guidance, Navigation, and Control Conference and Exhibit – volume: 13 start-page: 596 year: 1990 end-page: 602 ident: br0050 article-title: Near-optimal midcourse guidance for air-to-air missiles publication-title: J. Guid. Control Dyn. – volume: 56 start-page: 3655 year: 2020 end-page: 3673 ident: br0130 article-title: Midcourse guidance for exo-atmospheric interception using response surface based trajectory shaping publication-title: IEEE Trans. Aerosp. Electron. Syst. – volume: 19 start-page: 107 year: 1996 end-page: 112 ident: br0100 article-title: Strategic intercept midcourse guidance using modified zero effort miss steering publication-title: J. Guid. Control Dyn. – volume: 35 start-page: 645 year: 2012 end-page: 648 ident: br0200 article-title: Noniterative instantaneous impact point prediction algorithm for launch operations publication-title: J. Guid. Control Dyn. – start-page: 273 year: 2007 end-page: 298 ident: br0150 article-title: Tactical and Strategic Missile Guidance – volume: 37 start-page: 383 year: 2014 end-page: 390 ident: br0210 article-title: Analytic time derivatives of instantaneous impact point publication-title: J. Guid. Control Dyn. – volume: 18 start-page: 465 year: 1995 end-page: 470 ident: br0120 article-title: Optimal midcourse guidance law for fixed-interval propulsive maneuvers publication-title: J. Guid. Control Dyn. – volume: 43 start-page: 1711 year: 2020 end-page: 1722 ident: br0140 article-title: Midcourse guidance strategy for multistage interceptors with coasting phase publication-title: J. Guid. Control Dyn. – volume: 10 start-page: 61 issue: 1 year: 1987 ident: 10.1016/j.ast.2021.107159_br0060 article-title: Analytical solution of optimal trajectory-shaping guidance publication-title: J. Guid. Control Dyn. doi: 10.2514/3.20181 – volume: 22 start-page: 260 issue: 3 year: 2001 ident: 10.1016/j.ast.2021.107159_br0020 article-title: Exo-atmospheric intercepts: bringing new challenges to standard missile publication-title: Johns Hopkins APL Tech. Dig. – volume: 97 year: 2020 ident: 10.1016/j.ast.2021.107159_br0220 article-title: Autonomous ascent guidance with multiple terminal constraints for all-solid launch vehicles publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2019.105633 – volume: 56 start-page: 3655 issue: 5 year: 2020 ident: 10.1016/j.ast.2021.107159_br0130 article-title: Midcourse guidance for exo-atmospheric interception using response surface based trajectory shaping publication-title: IEEE Trans. Aerosp. Electron. Syst. doi: 10.1109/TAES.2020.2976084 – volume: 43 start-page: 1711 issue: 9 year: 2020 ident: 10.1016/j.ast.2021.107159_br0140 article-title: Midcourse guidance strategy for multistage interceptors with coasting phase publication-title: J. Guid. Control Dyn. doi: 10.2514/1.G005059 – volume: 37 start-page: 1 issue: 2 year: 2010 ident: 10.1016/j.ast.2021.107159_br0240 article-title: Algorithm 902: GPOPS, a Matlab software for solving multiple-phase optimal control problems using the Gauss pseudospectral method publication-title: ACM Trans. Math. Softw. doi: 10.1145/1731022.1731032 – volume: 86 start-page: 256 year: 2019 ident: 10.1016/j.ast.2021.107159_br0260 article-title: Output feedback continuous terminal sliding mode guidance law for missile-target interception with autopilot dynamics publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2019.01.012 – volume: 19 start-page: 280 year: 2014 ident: 10.1016/j.ast.2021.107159_br0230 article-title: Dynamic classification of ballistic missiles using neural networks and hidden Markov models publication-title: Appl. Soft Comput. doi: 10.1016/j.asoc.2014.02.015 – volume: 34 start-page: 860 issue: 3 year: 2011 ident: 10.1016/j.ast.2021.107159_br0080 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: 36 start-page: 958 issue: 4 year: 2013 ident: 10.1016/j.ast.2021.107159_br0250 article-title: Instantaneous impact point prediction using the response surface meth-od publication-title: J. Guid. Control Dyn. doi: 10.2514/1.59625 – volume: 2019 start-page: 1 year: 2019 ident: 10.1016/j.ast.2021.107159_br0170 article-title: Optimal midcourse guidance algorithm for exoatmospheric interception using analytical gradients publication-title: Int. J. Aerosp. Eng. doi: 10.1155/2019/8502870 – volume: 37 start-page: 214 issue: 1 year: 2014 ident: 10.1016/j.ast.2021.107159_br0070 article-title: Near-optimal spatial midcourse guidance law with an angular constraint publication-title: J. Guid. Control Dyn. doi: 10.2514/1.60356 – volume: 34 start-page: 60 issue: 9 year: 1997 ident: 10.1016/j.ast.2021.107159_br0010 article-title: Future challenges to ballistic missile defense publication-title: IEEE Spectr. doi: 10.1109/6.619381 – volume: 13 start-page: 596 issue: 4 year: 1990 ident: 10.1016/j.ast.2021.107159_br0050 article-title: Near-optimal midcourse guidance for air-to-air missiles publication-title: J. Guid. Control Dyn. doi: 10.2514/3.25375 – volume: 37 start-page: 383 issue: 2 year: 2014 ident: 10.1016/j.ast.2021.107159_br0210 article-title: Analytic time derivatives of instantaneous impact point publication-title: J. Guid. Control Dyn. doi: 10.2514/1.61681 – year: 1998 ident: 10.1016/j.ast.2021.107159_br0110 article-title: Exo-atmospheric intercept with J2 correction – volume: 9 start-page: 103 issue: 2 year: 1986 ident: 10.1016/j.ast.2021.107159_br0040 article-title: Advanced midcourse guidance for air to air missiles publication-title: J. Guid. Control Dyn. doi: 10.2514/3.20081 – volume: 76 start-page: 523 year: 2018 ident: 10.1016/j.ast.2021.107159_br0180 article-title: Near time-optimal feedback instantaneous impact point (IIP) guidance law for rocket publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2018.02.024 – volume: 19 start-page: 107 issue: 1 year: 1996 ident: 10.1016/j.ast.2021.107159_br0100 article-title: Strategic intercept midcourse guidance using modified zero effort miss steering publication-title: J. Guid. Control Dyn. doi: 10.2514/3.21586 – year: 1994 ident: 10.1016/j.ast.2021.107159_br0090 article-title: Exo-atmospheric intercept using modified proportional guidance with gravity correction for coast phase – volume: 43 start-page: 373 issue: 2 year: 2020 ident: 10.1016/j.ast.2021.107159_br0190 article-title: Instantaneous impact point guidance considering uncertainty in engine cutoff time publication-title: J. Guid. Control Dyn. doi: 10.2514/1.G004703 – volume: 18 start-page: 465 issue: 3 year: 1995 ident: 10.1016/j.ast.2021.107159_br0120 article-title: Optimal midcourse guidance law for fixed-interval propulsive maneuvers publication-title: J. Guid. Control Dyn. doi: 10.2514/3.21410 – volume: 32 start-page: 79 issue: 1 year: 2009 ident: 10.1016/j.ast.2021.107159_br0270 article-title: Integrated higher-order sliding mode guidance and autopilot for dual-control missiles publication-title: J. Guid. Control Dyn. doi: 10.2514/1.36961 – volume: 99 year: 2020 ident: 10.1016/j.ast.2021.107159_br0030 article-title: Reinforcement learning for angle-only intercept guidance of maneuvering targets publication-title: Aerosp. Sci. Technol. doi: 10.1016/j.ast.2020.105746 – volume: 27 start-page: 989 issue: 6 year: 2004 ident: 10.1016/j.ast.2021.107159_br0160 article-title: Lambert guidance routine designed to match position and velocity of ballistic target publication-title: J. Guid. Control Dyn. doi: 10.2514/1.1679 – volume: 33 start-page: 915 issue: 3 year: 2010 ident: 10.1016/j.ast.2021.107159_br0280 article-title: Attitude guidance for spinning vehicles with independent pitch and yaw control publication-title: J. Guid. Control Dyn. doi: 10.2514/1.44430 – start-page: 273 year: 2007 ident: 10.1016/j.ast.2021.107159_br0150 – volume: 35 start-page: 645 issue: 2 year: 2012 ident: 10.1016/j.ast.2021.107159_br0200 article-title: Noniterative instantaneous impact point prediction algorithm for launch operations publication-title: J. Guid. Control Dyn. doi: 10.2514/1.56395 |
| SSID | ssj0002942 |
| Score | 2.3449175 |
| Snippet | This paper proposes a noniterative feedback midcourse guidance algorithm for intercepting a ballistic target. The virtual impact point (VIP) concept, which is... |
| SourceID | crossref elsevier |
| SourceType | Enrichment Source Index Database Publisher |
| StartPage | 107159 |
| SubjectTerms | Ballistic target Exo-atmospheric interception Instantaneous impact point Midcourse guidance Missile defense |
| Title | Noniterative feedback midcourse guidance for exo-atmospheric interception of ballistic targets using virtual impact point steering |
| URI | https://dx.doi.org/10.1016/j.ast.2021.107159 |
| Volume | 119 |
| WOSCitedRecordID | wos000711641200004&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/eLvHCXMwtV1Lj9MwELZKlwMcEE-xvOQDJyKjPNo6Pga0CFZQIW2Reov8ytKlTaq-1L3yyxm_QugCAiQuVmvFceT5MjOezHxG6DlY1IzLvCKKJyMyAIeCcNOYOk2rD0VmC4Xf0_E4n07Zx15vF2phdnNa1_l-z5b_VdTQB8I2pbN_Ie72ptABv0Ho0ILYof0jwY_NW6oDoTcYJ8Hll2gxU7IxCRvR-XambJ2AJfveN4RvFs3asAvMpGWPCJkuxo8UfD63VM6RSxlfR1sbXNjNVrbwxBdZLhsYGAFgLLFh1-EtNJhhuEZHoYDIpmxeCeif2pDtq0vd1OfkU4vY4rOrHeF6cbn1d_YxijQ5yPdoi2c-wIbAqMHirKNyUxoTowacRXJ9sM0iWVCmQU-7v1d0vgs_XLzka5MbmybQQxNPM_4jlfaZmctMBftccLXY6Bo6SumQ5X10VLw7mZ62Njxl9til9tnC93CbGXgw0c89mo6XMrmNbvntBS4cLO6gnq7vopsd0sl76GsXIDgABLcAwQEgGACCDwCCuwDBTYVbgGAPEGwBgj1AsAMItgDBASD30eTNyeT1W-JP4iAyZXRD1IgnWsYypoxWlVZMaXi6SuZCDKXODadPJpnmTNAk4VRVVNFqBK6y1jLLdPYA9eum1g8RljwZ6KE5dSBRgypWTMSCZUIkTGR5nOtjFIfFLKVnqTeHpczLkI54UcL6l2b9S7f-x-hFO2TpKFp-d_EgSKj0uHe-Ywlw-vWwR_827DG68f11eIL6m9VWP0XX5W4zW6-eedB9AxoyqE0 |
| 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=Noniterative+feedback+midcourse+guidance+for+exo-atmospheric+interception+of+ballistic+targets+using+virtual+impact+point+steering&rft.jtitle=Aerospace+science+and+technology&rft.au=Jo%2C+Byeong-Un&rft.au=Ahn%2C+Jaemyung&rft.date=2021-12-01&rft.pub=Elsevier+Masson+SAS&rft.issn=1270-9638&rft.eissn=1626-3219&rft.volume=119&rft_id=info:doi/10.1016%2Fj.ast.2021.107159&rft.externalDocID=S1270963821006696 |
| 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 |