DC Field | Value | Language |
---|---|---|
dc.contributor.author | Mok, Sung-Hoon | ko |
dc.contributor.author | Choi, Yoon-Hyuk | ko |
dc.contributor.author | Bang, Hyo-Choong | ko |
dc.date.accessioned | 2013-03-11T16:24:03Z | - |
dc.date.available | 2013-03-11T16:24:03Z | - |
dc.date.created | 2012-02-06 | - |
dc.date.created | 2012-02-06 | - |
dc.date.issued | 2010-12 | - |
dc.identifier.citation | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.11, no.4, pp.351 - 359 | - |
dc.identifier.issn | 1229-9626 | - |
dc.identifier.uri | http://hdl.handle.net/10203/99592 | - |
dc.description.abstract | This paper proposes a linear system control algorithm with collision avoidance in multiple satellites. Consideration of collision avoidance is augmented by adding a weighting term in the cost function of the original tracking problem in linear quadratic control (LQC). Because the proposed algorithm relies on a similar solution procedure to the original LQC, its inherent advantages, including gain-robustness and optimality, are preserved. To confirm and visualize the derived algorithm, a simple example of two-vehicle motion in the two-dimensional plane is illustrated. In addition, the proposed collision avoidance control is applied to satellite formation flying, and verified by numerical simulations. | - |
dc.language | English | - |
dc.publisher | 한국항공우주학회 | - |
dc.title | Collision avoidance using linear quadratic control in satellite formation flying | - |
dc.type | Article | - |
dc.type.rims | ART | - |
dc.citation.volume | 11 | - |
dc.citation.issue | 4 | - |
dc.citation.beginningpage | 351 | - |
dc.citation.endingpage | 359 | - |
dc.citation.publicationname | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES | - |
dc.contributor.localauthor | Bang, Hyo-Choong | - |
dc.contributor.nonIdAuthor | Mok, Sung-Hoon | - |
dc.contributor.nonIdAuthor | Choi, Yoon-Hyuk | - |
dc.description.isOpenAccess | N | - |
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