DC Field | Value | Language |
---|---|---|
dc.contributor.advisor | Bang, Hyochoong | - |
dc.contributor.advisor | 방효충 | - |
dc.contributor.author | Kwon, Dong Young | - |
dc.date.accessioned | 2023-06-23T19:35:02Z | - |
dc.date.available | 2023-06-23T19:35:02Z | - |
dc.date.issued | 2022 | - |
dc.identifier.uri | http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=996309&flag=dissertation | en_US |
dc.identifier.uri | http://hdl.handle.net/10203/309336 | - |
dc.description | 학위논문(박사) - 한국과학기술원 : 항공우주공학과, 2022.2,[vi, 73 p. :] | - |
dc.description.abstract | An on-board guidance generation approach for Mars pinpoint landing is proposed based on so-called RT-SCP (Real-Time Sequential Convex Programming) formulation. To take into account optimal flight time in the formulation, a discretized form of the landing problem is linearized with respect to not only states and control, but also time increment. To implement this strategy in real-time, on-board demonstrations with GR740, which is next generation on-board processor of ESA, are conducted. From the demonstration results, the total number of time steps for real-time operation is determined. Numerical simulation results indicate that the proposed strategy well follows the optimal solution from GPOPS-II under no disturbance condition. | - |
dc.language | eng | - |
dc.publisher | 한국과학기술원 | - |
dc.title | Sequential convex programming approach for real-time guidance during the powered descent phase of Mars landing missions | - |
dc.title.alternative | 화성 착륙 임무의 동력 하강 단계 동안의 실시간 유도를 위한 순차 볼록 프로그래밍 방식 연구 | - |
dc.type | Thesis(Ph.D) | - |
dc.identifier.CNRN | 325007 | - |
dc.description.department | 한국과학기술원 :항공우주공학과, | - |
dc.contributor.alternativeauthor | 권동영 | - |
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