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| 2 |
Vaddi， S. S., Vadali, S. R. and Alfriend, K. T., 2003, "Formation Flying:Accommodating Nonlinearity and Eccentricity Perturbations", Joumal of Guidance, Control and Dynamics, Vol. 26, No. 2, pp. 214-223/
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Young-Hyun Kim, Seung-Won Seo, Nam-Sook Chung and Young-Keun Chang, "Three- Axis Attitude Stabilization System Design of Picosatellite HAUSAT-1," CubeSat Symposium Papers, 1st Intemational CubeSat Symposium, Tokyo, Japan, 2003./
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| 4 |
"CUBESAT Design Specifications Document," Revision VII, February, 2003./
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| 5 |
Young-Hyun Kim and Young-Keun Chang, "Development of HAUSAT-1 Picosatellite (CubeSat) for Educational Purpose," CubeSat Symposium Papers, 1st Intemational CubeSat Symposium, Tokyo, Japan, 2003./
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Choi, J. M., Kim, H. K., and Hyun, B. S., 2003, " Therrnal Ana1ysis on Satellite during Launch Stage by Analytical Solution", Proceedings of the KSAS Spring Annual Meeting, pp. 694-697/
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Kim, D. H., Park, Y. M. Lee, I. and Kwon O. J., "Nonlinear Aeroelastic Computation of a Wing with a Finned-Store Using a Parallel Unstructured Euler Solver", 43nd AlAN ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf. & Exhibit, Denver, Colorado, 22-25 April 2002, AIAA Paper 1289./
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| 8 |
Sohn, M. H. and Lee, K Y., "Experimental Investigation of Vortex Flow of a Yawed Delta Wing Having Leading Edge Extension", AIAA Paper 2002-3267, June 2002./
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| 9 |
Sang Wook Lee and Oh loon Kwon, "Aerodynamic Shape Optimization Using a Continuous Adjoint Formulation on Unstructured Meshes," J. of KSAS, Vol. 30, No. 4, 2002, pp. 18-27./
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| 10 |
Sangho Kim, Alonso, J. J., and Jameson, A., "Design Optimization of High- Lift Configurations Using a Viscous Continuous Adjoint Method," AIAA-2002-0844, 2002./
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