Improvement of satellite system integration process based on dummy panel method더미패널을 이용한 인공위성 시스템 통합 절차 개선

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This thesis proposes a new methodology for the innovative improvement of satellite system integration procedures. To overcome the limitations of traditional sequential procedures, a novel integration process utilizing dummy panels has been developed. This innovative approach, grounded in practical project experience, has been successfully applied in significant real-world projects, including the Geo-Kompsat 2 (GK2) and the Korea Pathfinder Lunar Orbiter (KPLO) development projects. This practical success demonstrates the potential for revolutionizing conventional methodologies in the field of satellite system integration, marking an important milestone for future advancements in this area. The dummy-panel process represents a significant departure from the traditional Flight Model (FM-panel) process, showcasing a new direction in satellite system integration and testing. The study’s centerpiece is a comprehensive analysis of the dummy-panel process, employing Design Structure Matrix (DSM) based modeling and simulation techniques. In developing the simulation model, extensive research was conducted into various project facets. This research included detailed evaluations of task dependencies, duration and cost estimates, the likelihood of rework, and the repercussions of such changes. Inputs for these simulations were derived from actual project data, ensuring both accuracy and relevance. Subsequent discrete event simulations, powered by a custom-developed algorithm, meticulously replicated the project execution process. This algorithm accurately simulates a range of scenarios, including sequential, parallel, and overlapping tasks, along with both feedback and feedforward rework processes, thus offering a holistic view of project dynamics. The results of the simulations and sensitivity analyses in this study act as practical case studies, yielding critical insights into the performance of each process, encompassing total duration and cost distributions. These analyses are pivotal in gauging schedule and cost risks and in understanding how variations in process architecture affect the project. Insights from these case studies are key in optimizing project schedules and formulating effective risk management strategies. They underscore the criticality of comprehending task interdependencies and their substantial impact on project outcomes. Moreover, these analyses highlight the crucial balance between cost and project duration, stressing the need for identifying and implementing optimal execution strategies. This research shows that despite the dummy-panel process typically requiring a somewhat higher cost, it can be a more preferred method in environments with low risk tolerance, due to its more predictable outcomes and effective risk management capabilities. By combining practical insights gained from important projects with the analytical depth of DSM-based simulation methods, a powerful framework for improving the satellite development process is provided. Future studies should aim to encompass a broader range of processes and investigate the dynamic nature of task dependencies that may change during the course of a project.
Advisors
안재명researcher
Description
한국과학기술원 :항공우주공학과,
Publisher
한국과학기술원
Issue Date
2024
Identifier
325007
Language
eng
Description

학위논문(박사) - 한국과학기술원 : 항공우주공학과, 2024.2,[v, 89 p. :]

Keywords

더미패널▼a프로젝트관리▼a시스템 통합▼a디자인 구조 행렬 모델▼a이산 이벤트 시뮬레이션▼a절충연구; Dummy panel▼aProject management▼aSystem integration▼aDesign structure matrix▼aDiscrete event simulation▼aTrade-off study

URI
http://hdl.handle.net/10203/322223
Link
http://library.kaist.ac.kr/search/detail/view.do?bibCtrlNo=1100137&flag=dissertation
Appears in Collection
AE-Theses_Ph.D.(박사논문)
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