DC Field | Value | Language |
---|---|---|
dc.contributor.author | Ann, Sungjun | ko |
dc.contributor.author | Lee, Seokwon | ko |
dc.contributor.author | Kim, Youdan | ko |
dc.contributor.author | Ahn, Jaemyung | ko |
dc.date.accessioned | 2020-11-16T02:55:12Z | - |
dc.date.available | 2020-11-16T02:55:12Z | - |
dc.date.created | 2020-11-03 | - |
dc.date.created | 2020-11-03 | - |
dc.date.issued | 2020-10 | - |
dc.identifier.citation | IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, v.56, no.5, pp.3655 - 3673 | - |
dc.identifier.issn | 0018-9251 | - |
dc.identifier.uri | http://hdl.handle.net/10203/277288 | - |
dc.description.abstract | An exoatmospheric midcourse guidance law is proposed to intercept a ballistic missile during the free-flight phase. The proposed guidance law generates a thrust direction command for an antiballistic missile to hit the target at the predicted intercept point. For the predicted intercept point, the zero-effort-miss and zero-effort-velocity are determined based on the solutions of the two-body orbital boundary/initial value problems. The intercept point is predicted by using the trajectory shaping parameter that combines the zero effort trajectory and minimum time trajectory. A response surface model for the minimum interception time is constructed as a database, which is the polynomial function of the initial condition. The response surface model provides a predicted minimum time interception position for the midcourse guidance. Case studies are performed to demonstrate the performance of the proposed guidance law considering various uncertainties. | - |
dc.language | English | - |
dc.publisher | IEEE-INST ELECTRICAL ELECTRONICS ENGINEERS INC | - |
dc.title | Midcourse Guidance for Exoatmospheric Interception Using Response Surface Based Trajectory Shaping | - |
dc.type | Article | - |
dc.identifier.wosid | 000578773300023 | - |
dc.identifier.scopusid | 2-s2.0-85079869605 | - |
dc.type.rims | ART | - |
dc.citation.volume | 56 | - |
dc.citation.issue | 5 | - |
dc.citation.beginningpage | 3655 | - |
dc.citation.endingpage | 3673 | - |
dc.citation.publicationname | IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS | - |
dc.identifier.doi | 10.1109/TAES.2020.2976084 | - |
dc.contributor.localauthor | Ahn, Jaemyung | - |
dc.contributor.nonIdAuthor | Ann, Sungjun | - |
dc.contributor.nonIdAuthor | Lee, Seokwon | - |
dc.contributor.nonIdAuthor | Kim, Youdan | - |
dc.description.isOpenAccess | N | - |
dc.type.journalArticle | Article | - |
dc.subject.keywordAuthor | Missiles | - |
dc.subject.keywordAuthor | Response surface methodology | - |
dc.subject.keywordAuthor | Trajectory | - |
dc.subject.keywordAuthor | Uncertainty | - |
dc.subject.keywordAuthor | Rockets | - |
dc.subject.keywordAuthor | Atmospheric modeling | - |
dc.subject.keywordAuthor | Antiballistic Missile | - |
dc.subject.keywordAuthor | Exoatmospheric Environment | - |
dc.subject.keywordAuthor | Midcourse Guidance Law | - |
dc.subject.keywordAuthor | Response Surface Methodology | - |
dc.subject.keywordAuthor | Solid Propellant Rocket | - |
dc.subject.keywordAuthor | Trajectory Optimization | - |
dc.subject.keywordAuthor | Trajectory Shaping | - |
dc.subject.keywordPlus | NEURAL-NETWORKS | - |
dc.subject.keywordPlus | MISSILES | - |
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