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테더가 있는 인공위성의 비선형 동역학 해석Nonlinear Dynamic Analysis of a Tethered Satellite
- Other Titles
- Nonlinear Dynamic Analysis of a Tethered Satellite
- Issue Date
- May-2011
- Publisher
- 한국소음진동공학회
- Keywords
- Nonlinear Dynamics; Tethered Satellite; Time Integration; 비선형 동역학; 테더가 있는 인공위성; 시간적분법
- Citation
- 한국소음진동공학회논문집, v.21, no.5, pp 416 - 421
- Pages
- 6
- Indexed
- KCI
- Journal Title
- 한국소음진동공학회논문집
- Volume
- 21
- Number
- 5
- Start Page
- 416
- End Page
- 421
- ISSN
- 1598-2785
2287-5476
- Abstract
- The purpose of this study is to analyze nonlinear dynamics of a tethered satellite. The nonlinear equations of motion are derived by using Lagrange's equations with the polar coordinate system. In order to analyze the response of tethered satellite, time responses are computed by the Newmark’s time integration method. This paper claims that the dynamic behavior of the system is changed by the effect of length of tether, mass ratio of satellites.
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Related Researcher
- Chung, Jintai
- ERICA 공학대학 (DEPARTMENT OF MECHANICAL ENGINEERING)