Electromagnetic Compatibility Design for KOMPSAT-2

Journal of Astronomy and Space Sciences

Na-Young Lee¹  Jin-Ho Lee¹ 

[1] Korea Aerospace Research Institute, 45 Youseong, Daejon 305-333, Korea;

关键词: KOMPSAT-2;    electro-magnetic compatibility;    conducted emission;    conducted susceptibility;    radiated emission;    radiated susceptibility;    spacecraft;   

DOI  :  10.5140/JASS.2003.20.4.383

来源: DOAJ

【 摘 要 】

It is quite essential that requirements allocation and analysis would be done for the electromagnetic compatibility (EMC) of all units when designing a satellite. Although KOMPSAT-2 inherits relatively large portions of the electrical designs from KOMPSAT-1, it has a new instrument and different combinations of sensors and actuators as well as their driving circuitry. Many requirements for the electromagnetic compatibility were modified and newly allocated for KOMPSAT-2. Naturally, they must be justified through analyses from the early stage of the program. In this paper, the EMC compatibility requirements for KOMPSAT2 are presented and verified for their suitability. In addition, some results, which were obtained from various analyses, are presented and discussed.

【 授权许可】

Unknown