1 |
Gordji RR, Morgan ZCPO, Di SL, Processor, payload, and power subsystem development of the MISSat-1 CubeSat, PhD Dissertation, The University of Mississippi (2014).
|
2 |
Jeon MJ, Lee NY, Kim DY, Kim GS, Implementation of a power simulator for energy balance analysis of a LEO satellite, Aerosp. Eng. Technol. 9, 176-184 (2010).
|
3 |
Kim DW, Design improvement and performance optimization of HAUSAT-2 Nano satellite electrical power subsystem, Master Dissertation, Korea Aerospace University (2007).
|
4 |
Kim HD, Choi WS, Cho DH, Kim MK, Kim JH, et al., Current status of the development of 6U Cubesat for high resolution image and video (HiREV Cubesat), Proceedings of the KSAS 2016 Fall Conference, 444-445 (2016).
|
5 |
Lee SK, Ra SW, Development of energy balance analysis program for LEO satellite design, J. Korean Soc. Aeronaut. Space Sci. 35, 850-857 (2007). https://doi.org/10.5139/JKSAS.2007.35.9.850
|
6 |
Seong JD, Kim HD, Lim SM, An analysis of three-dimensional collision probability according to approaching objects to the KOMPSAT series, J. Korean Soc. Aeronaut. Space Sci. 41, 156-163 (2013). https://doi.org/10.5139/JKSAS.2013.41.2.156
|