서브메뉴
검색
Robust Optimal Entry Guidance for Future Mars Landers
Robust Optimal Entry Guidance for Future Mars Landers
상세정보
- 자료유형
- 학위논문파일 국외
- ISBN
- 9798522971755
- DDC
- 629.1
- 서명/저자
- Robust Optimal Entry Guidance for Future Mars Landers
- 발행사항
- [Sl] : University of California, Irvine, 2021
- 발행사항
- Ann Arbor : ProQuest Dissertations & Theses, 2021
- 형태사항
- 137 p
- 주기사항
- Source: Dissertations Abstracts International, Volume: 83-02, Section: A.
- 주기사항
- Advisor: Mease, Kenneth D.
- 학위논문주기
- Thesis (Ph.D.)--University of California, Irvine, 2021.
- 사용제한주기
- This item must not be sold to any third party vendors.
- 일반주제명
- Aerospace engineering
- 일반주제명
- Robotics
- 일반주제명
- Engineering
- 일반주제명
- Laboratories
- 일반주제명
- Control theory
- 일반주제명
- Standard deviation
- 일반주제명
- Monte Carlo simulation
- 일반주제명
- Velocity
- 일반주제명
- Accuracy
- 일반주제명
- Random variables
- 일반주제명
- Sensitivity analysis
- 일반주제명
- Atmosphere
- 일반주제명
- Optimization
- 일반주제명
- Altitude
- 일반주제명
- Teaching assistants
- 일반주제명
- Design
- 일반주제명
- Algorithms
- 일반주제명
- Designers
- 키워드
- Entry phase
- 키워드
- High mass
- 키워드
- Lading ellipse
- 기타저자
- University of California, Irvine Mechanical and Aerospace Engineering - PhD
- 기본자료저록
- Dissertations Abstracts International. 83-02A.
- 기본자료저록
- Dissertation Abstract International
- 전자적 위치 및 접속
- 로그인 후 원문을 볼 수 있습니다.
MARC
008220131s2021 us c eng d■020 ▼a9798522971755
■035 ▼a(MiAaPQ)AAI28545122
■040 ▼aMiAaPQ▼cMiAaPQ
■0820 ▼a629.1
■1001 ▼aNoyes, Connor David.
■24510▼aRobust Optimal Entry Guidance for Future Mars Landers
■260 ▼a[Sl]▼bUniversity of California, Irvine▼c2021
■260 1▼aAnn Arbor▼bProQuest Dissertations & Theses▼c2021
■300 ▼a137 p
■500 ▼aSource: Dissertations Abstracts International, Volume: 83-02, Section: A.
■500 ▼aAdvisor: Mease, Kenneth D.
■5021 ▼aThesis (Ph.D.)--University of California, Irvine, 2021.
■506 ▼aThis item must not be sold to any third party vendors.
■590 ▼aSchool code: 0030.
■650 4▼aAerospace engineering
■650 4▼aRobotics
■650 4▼aEngineering
■650 4▼aLaboratories
■650 4▼aControl theory
■650 4▼aStandard deviation
■650 4▼aMonte Carlo simulation
■650 4▼aVelocity
■650 4▼aAccuracy
■650 4▼aRandom variables
■650 4▼aSensitivity analysis
■650 4▼aAtmosphere
■650 4▼aOptimization
■650 4▼aAltitude
■650 4▼aTeaching assistants
■650 4▼aDesign
■650 4▼aAlgorithms
■650 4▼aDesigners
■653 ▼aEntry phase
■653 ▼aHigh mass
■653 ▼aLading ellipse
■653 ▼aHigher elevation landing
■690 ▼a0538
■690 ▼a0771
■690 ▼a0537
■690 ▼a0389
■71020▼aUniversity of California, Irvine▼bMechanical and Aerospace Engineering - Ph.D..
■7730 ▼tDissertations Abstracts International▼g83-02A.
■773 ▼tDissertation Abstract International
■790 ▼a0030
■791 ▼aPh.D.
■792 ▼a2021
■793 ▼aEnglish
■85640▼uhttp://www.riss.kr/pdu/ddodLink.do?id=T16052621▼nKERIS▼z이 자료의 원문은 한국교육학술정보원에서 제공합니다.
■980 ▼a202202▼f2022


