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High-Fidelity Simulation of Small-Body Lander/Rover Spacecraft
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| 자료유형 | 학위논문 |
|---|---|
| 서명/저자사항 | High-Fidelity Simulation of Small-Body Lander/Rover Spacecraft. |
| 개인저자 | Van wal, Stefaan. |
| 단체저자명 | University of Colorado at Boulder. Aerospace Engineering. |
| 발행사항 | [S.l.]: University of Colorado at Boulder., 2018. |
| 발행사항 | Ann Arbor: ProQuest Dissertations & Theses, 2018. |
| 형태사항 | 338 p. |
| 기본자료 저록 | Dissertation Abstracts International 80-02B(E). Dissertation Abstract International |
| ISBN | 9780438382503 |
| 학위논문주기 | Thesis (Ph.D.)--University of Colorado at Boulder, 2018. |
| 일반주기 |
Source: Dissertation Abstracts International, Volume: 80-02(E), Section: B.
Adviser: Daniel J. Scheeres. |
| 요약 | The scientific return of spacecraft missions that explore solar system small bodies can be increased through the inclusion of surface exploration with deployed probes. In this dissertation, a methodology is presented that allows for fast, parall |
| 요약 | The coarse small-body shape is modeled using an implicit signed distance field (SDF) that allows for fast collision detection. Statistical features are included onto the SDF using procedural generation techniques. The small-body gravity field is |
| 요약 | The developed simulation framework is applied to perform parametric investigations of probe deployment, which quantify the effects of relevant properties of a probe and its target small body. The probe shape and internal mass distribution are fo |
| 요약 | Finally, the framework is applied to perform a pre-arrival deployment analysis of the MINERVA-II rovers onboard the Hayabusa-2 spacecraft. This analysis identified challenges in the rover deployment and was used to redesign aspects of the nomina |
| 일반주제명 | Aerospace engineering. |
| 언어 | 영어 |
| 바로가기 | 
: 이 자료의 원문은 한국교육학술정보원에서 제공합니다. |
