위성발사체의 궤적최적화와 최적유도 알고리듬 설계
- Title
- 위성발사체의 궤적최적화와 최적유도 알고리듬 설계
- Other Titles
- Trajectory Optimization and Optimal Explicit Guidance Algorithm Design for a Satellite Launch Vehicle
- Author
- 송택렬
- Keywords
- satellite; launch vehicle; trajectory; optimization; optimal guidance; explicit guidance; algorithm
- Issue Date
- 2001-02
- Publisher
- 제어로봇시스템학회
- Citation
- 제어로봇시스템학회 논문지, v. 7, no. 2, page. 173-182
- Abstract
- Ascent trajectory optimization and optimal explicit guidance problems for a satellite launch vehicle in a 2-dimensional pitch plane are studied. The trajectory optimization problem wiLh boundary condilions is formulated as a nonlinear programming problem by parameterizing the pitch attitude control variable, and is solved by using the SQP algorithm. The flight constraints such as gravity-tum are imposed. An optimal explicit guidance algorithm in the exoatmospheric phase is also presented, the guidance algorithm provides steering command and time-to-go value directly using the current states of the vehicle and the desired orbit insertion conditions. To verify the optimality and accuracy of the algorithm, numerical simulations are performed.
- URI
- https://www.dbpia.co.kr/journal/articleDetail?nodeId=NODE01964720https://repository.hanyang.ac.kr/handle/20.500.11754/158687
- ISSN
- 1976-5622; 2233-4335
- Appears in Collections:
- COLLEGE OF ENGINEERING SCIENCES[E](공학대학) > ELECTRICAL ENGINEERING(전자공학부) > Articles
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