DC Field | Value | Language |
---|---|---|
dc.contributor.author | Ahn, Jaemyung | ko |
dc.contributor.author | Wang, Pengyu | ko |
dc.contributor.author | Guo, Yanning | ko |
dc.contributor.author | Wie, Bong | ko |
dc.date.accessioned | 2019-12-13T08:22:31Z | - |
dc.date.available | 2019-12-13T08:22:31Z | - |
dc.date.created | 2019-07-31 | - |
dc.date.created | 2019-07-31 | - |
dc.date.issued | 2019-06 | - |
dc.identifier.citation | Astrodynamics, v.3, no.2, pp.127 - 136 | - |
dc.identifier.issn | 2522-008X | - |
dc.identifier.uri | http://hdl.handle.net/10203/269084 | - |
dc.description.abstract | This paper investigates a problem of determining the optimal terminal-time or time-to-go of the ZEM/ZEV (Zero-Effort-Miss/Zero-Effort-Velocity) feedback guidance law for a variety of orbital intercept or rendezvous maneuvers. A generalized ZEM/ZEV guidance problem, whose objective is to minimize a combination of the control energy and terminal time, is examined. Algebraic equations whose solution provides the optimal terminal-time of the orbital intercept/rendezvous problems are derived based on the optimal control theory. The effectiveness of the proposed approach is demonstrated for various orbital maneuver problems. | - |
dc.language | English | - |
dc.publisher | Springer Science and Business Media LLC | - |
dc.title | Optimal terminal-time determination for the ZEM/ZEV feedback guidance law with generalized performance index | - |
dc.type | Article | - |
dc.identifier.scopusid | 2-s2.0-85081738262 | - |
dc.type.rims | ART | - |
dc.citation.volume | 3 | - |
dc.citation.issue | 2 | - |
dc.citation.beginningpage | 127 | - |
dc.citation.endingpage | 136 | - |
dc.citation.publicationname | Astrodynamics | - |
dc.identifier.doi | 10.1007/s42064-019-0039-x | - |
dc.contributor.localauthor | Ahn, Jaemyung | - |
dc.contributor.nonIdAuthor | Wang, Pengyu | - |
dc.contributor.nonIdAuthor | Guo, Yanning | - |
dc.contributor.nonIdAuthor | Wie, Bong | - |
dc.description.isOpenAccess | N | - |
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