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http://dx.doi.org/10.5139/JKSAS.2003.31.4.053

A Study on the Solar Panel Deployment of a Satellite  

Seo, Jong Hwi (아주대학교)
Han, Sang Won (아주대학교)
Park, Tae Won (아주대학교)
Chae, Jang Su (한국항공우주산업(주))
Seo, Hyeon Seok (한국항공우주산업(주))
Publication Information
Journal of the Korean Society for Aeronautical & Space Sciences / v.31, no.4, 2003 , pp. 53-59 More about this Journal
Abstract
Strain Energy Hinge(SEH) has been used in Korea Multi-purpose Satellite(KOMPSAT) series to deploy the solar panel due to the good record of reliability. However, when it reached a desired deployment position, a large buckling force is applied to the main body. This may cause structural damage and also affect control of the satellite. Therefore, reliable dynamic analysis for the deployment system is required at a design stage. Moreover, various mission of a satellite has made the size of solar panels got bigger, so elastic effect has to be considered seriously to get more precise analysis results. In this paper, a dynamic analysis method to predict the deployment is verified by KOMPSAT-2 deployment test.
Keywords
Strain Energy Hinge; Solar Panel; Satellite; KOMPSAT; Deployment Analysis; Component Mode Synthesis; Normal Mode; Static Mode;
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  • Reference
1 Haug E.J., Computer-Aided Kinematics and Dynamics of Mechanical Systems, Volume 1: Basic Methods, Allyn and Bacon, MA, 1989.
2 라완규, 곽문규, "변형에너지 힌지를 갖는 인공위성 태양판 전개 모델 연구", 소음진동공학회 추계학술대회논문집, 1998, pp.280-284.
3 Wu S.C., Haug E.J. and Kim S.S., "A Variational Approach to Dynamics of Flexible Multibody Systems", Technical Report 86-15, CCAD, Univ. of IOWA, 1986.
4 A. MUNJIA, "An $M(M^{-1}K)^m$ proportional damping in explicit integration of dynamics structural systems", International Journal for Numerical Methods in Engineering, Vol. 41, No.7, 1998, pp.1277-1296.   DOI   ScienceOn
5 곽문규, 라완규, "점탄성 변형에너지 힌지를 이용한 인공위성 태양판 전개장치 개발", 소음진동공학회 추계학술대회논문집, 1998, pp.285-289.
6 DADS/Flex Reference Manual, LMS CADSI, 1999.
7 MSC/NSATRAN DMAP Manual, The MacNeal-Schwendler Corporation.
8 Michael R and Mark M., MSC/NASTRAN Quick Reference Guide Version 70.5, The MacNeal-Schwendler Corporation.
9 김진철, 김학정 외, "아리랑 1호 위성의 개발기술", 한국항공우주학회지, Vol. 28, No.4, 2000, pp.143-162.
10 Kim S.S. and Haug E.J., "Selection of Deformation Modes for Flexible Multibody Dynamics", Mechanics of Structures and Machines Vol.18, No.4, 1990, pp.565-586.   DOI
11 박태원, 정원선, "Strain Energy Hinge 좌굴해석", 대한기계학회 춘계학술대회논문집, 2002, pp.468-474.
12 Spanos J.T. and Tsuha W.S., "Selection of Component Modes for Flexible Multibody Simulation", Journal of Guidance Vol.14, No.2, 1991, pp.278-286.   DOI
13 채장수, 황도순, "태양전지판 전개장치의 실험적 연구", 한국자동제어학술회의논문집, 1993, pp.778-782.
14 박태원, 서종휘, "태양전지판의 전개거동해석", DADS User's Conference, 2002.
15 Yoo W.S. and Haug E.J., "Dynamics of Flexible Mechanical Systems using Vibration and Static Correction Modes", Journal of Mech. Trans. Auto. Des 108, 1986, pp.315-322.   DOI
16 Shin S.S., Yoo W.S. and Tang J., "Effect of Mode Selection, Scailing, and Orthogonalization on the Dynamic Analysis of Flexible Multibody Systems", Mechanics of Structures and machines Vol.21, No.4, 1993, pp.507-527.   DOI