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Linear and Multilinear Methods for Guidance, Navigation, and Control of Satellite Formation Flight
Linear and Multilinear Methods for Guidance, Navigation, and Control of Satellite Formation Flight
Detailed Information
- 자료유형
- 학위논문 서양
- 최종처리일시
- 20250211152037
- ISBN
- 9798384050001
- DDC
- 519
- 저자명
- Kulik, Jackson.
- 서명/저자
- Linear and Multilinear Methods for Guidance, Navigation, and Control of Satellite Formation Flight
- 발행사항
- [Sl] : Cornell University, 2024
- 발행사항
- Ann Arbor : ProQuest Dissertations & Theses, 2024
- 형태사항
- 187 p
- 주기사항
- Source: Dissertations Abstracts International, Volume: 86-03, Section: B.
- 주기사항
- Advisor: Savransky, Dmitry.
- 학위논문주기
- Thesis (Ph.D.)--Cornell University, 2024.
- 초록/해제
- 요약Guidance, navigation, and control of satellites-especially in the study of rendezvous and formation flight-relies heavily on methods that leverage local linear approximations of dynamical systems and measurement functions. This thesis focuses mainly on cases in which linear approximations are insufficient to solve dynamics, control, or estimation problems. In such cases, we employ tools from numerical multilinear algebra on tensors arising from higher-order Taylor series. The inherently quadratic nature of some quantities, the linear unobservability of some estimation problems, and the need to quantify the performance of linear methods make these higher-order techniques useful in the setting of guidance, navigation, and control.
- 일반주제명
- Applied mathematics
- 일반주제명
- Aerospace engineering
- 일반주제명
- Astronomy
- 키워드
- Control
- 키워드
- Dynamics
- 키워드
- Guidance
- 키워드
- Navigation
- 키워드
- Rendezvous
- 키워드
- Tensor
- 기타저자
- Cornell University Applied Mathematics
- 기본자료저록
- Dissertations Abstracts International. 86-03B.
- 전자적 위치 및 접속
- 로그인 후 원문을 볼 수 있습니다.
MARC
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■020 ▼a9798384050001
■035 ▼a(MiAaPQ)AAI31335694
■040 ▼aMiAaPQ▼cMiAaPQ
■0820 ▼a519
■1001 ▼aKulik, Jackson.▼0(orcid)0009-0007-0740-0436
■24510▼aLinear and Multilinear Methods for Guidance, Navigation, and Control of Satellite Formation Flight
■260 ▼a[Sl]▼bCornell University▼c2024
■260 1▼aAnn Arbor▼bProQuest Dissertations & Theses▼c2024
■300 ▼a187 p
■500 ▼aSource: Dissertations Abstracts International, Volume: 86-03, Section: B.
■500 ▼aAdvisor: Savransky, Dmitry.
■5021 ▼aThesis (Ph.D.)--Cornell University, 2024.
■520 ▼aGuidance, navigation, and control of satellites-especially in the study of rendezvous and formation flight-relies heavily on methods that leverage local linear approximations of dynamical systems and measurement functions. This thesis focuses mainly on cases in which linear approximations are insufficient to solve dynamics, control, or estimation problems. In such cases, we employ tools from numerical multilinear algebra on tensors arising from higher-order Taylor series. The inherently quadratic nature of some quantities, the linear unobservability of some estimation problems, and the need to quantify the performance of linear methods make these higher-order techniques useful in the setting of guidance, navigation, and control.
■590 ▼aSchool code: 0058.
■650 4▼aApplied mathematics
■650 4▼aAerospace engineering
■650 4▼aAstronomy
■653 ▼aControl
■653 ▼aDynamics
■653 ▼aGuidance
■653 ▼aNavigation
■653 ▼aRendezvous
■653 ▼aTensor
■690 ▼a0364
■690 ▼a0538
■690 ▼a0606
■71020▼aCornell University▼bApplied Mathematics.
■7730 ▼tDissertations Abstracts International▼g86-03B.
■790 ▼a0058
■791 ▼aPh.D.
■792 ▼a2024
■793 ▼aEnglish
■85640▼uhttp://www.riss.kr/pdu/ddodLink.do?id=T17162648▼nKERIS▼z이 자료의 원문은 한국교육학술정보원에서 제공합니다.
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