• Àüü
  • ÀüÀÚ/Àü±â
  • Åë½Å
  • ÄÄÇ»ÅÍ
´Ý±â

»çÀÌÆ®¸Ê

Loading..

Please wait....

±¹³» ³í¹®Áö

Ȩ Ȩ > ¿¬±¸¹®Çå > ±¹³» ³í¹®Áö > Çѱ¹Á¤º¸Ã³¸®ÇÐȸ ³í¹®Áö > Á¤º¸Ã³¸®ÇÐȸ ³í¹®Áö ¼ÒÇÁÆ®¿þ¾î ¹× µ¥ÀÌÅÍ °øÇÐ

Á¤º¸Ã³¸®ÇÐȸ ³í¹®Áö ¼ÒÇÁÆ®¿þ¾î ¹× µ¥ÀÌÅÍ °øÇÐ

Current Result Document :

ÇѱÛÁ¦¸ñ(Korean Title) H-IMA : ºñÇà ¼ÒÇÁÆ®¿þ¾îÀÇ À̽ļº Çâ»óÀ» À§ÇÑ IMA ±â¹ÝÀÇ È¥ÇÕÇü Ç÷§Æû ¾ÆÅ°ÅØó
¿µ¹®Á¦¸ñ(English Title) H-IMA : IMA based Hybrid Platform Architecture for Improving Portability of Flight Software
ÀúÀÚ(Author) ¼­¿ëÁø   À±»óÇÊ   Á¶Çö¿ì   ±Çö¼ø   ±èÇü½Å   ±èÇö¼ö   Yongjin Seo   Sangpil Yun   Hyunwoo Joe   Cheolsoon Kwon   Hyungshin Kim   Hyeon Soo Kim  
¿ø¹®¼ö·Ïó(Citation) VOL 03 NO. 01 PP. 0007 ~ 0018 (2014. 01)
Çѱ۳»¿ë
(Korean Abstract)
ºñÇà ¼ÒÇÁÆ®¿þ¾î´Â ÀΰøÀ§¼ºÀÇ Å¾Àç ÄÄÇ»ÅÍ¿¡¼­ »ç¿ëµÇ´Â ¼ÒÇÁÆ®¿þ¾î·Î, ½Ç½Ã°£¼º°ú °í½Å·Ú¼ºÀÌ ¿ä±¸µÈ´Ù. ÀÌ¿Í °°Àº ¿ä±¸»çÇ×À¸·Î ÀÎÇØ ºñÇà ¼ÒÇÁÆ®¿þ¾î´Â µ¿ÀÛ È¯°æ¿¡ ´ëÇÑ Á¾¼Ó¼ºÀ» °®°Ô µÈ´Ù. ÀÌ·¯ÇÑ ¹®Á¦´Â »õ·Î¿î ½Ã½ºÅÛÀ» ±¸ÃàÇÒ ¶§¸¶´Ù ¸Å¹ø ´Ù½Ã °³¹ßÇÏ¿©¾ß ÇÏ´Â »óȲÀ» ÃÊ·¡ÇÑ´Ù. µû¶ó¼­ ºñÇà ¼ÒÇÁÆ®¿þ¾î¿Í µ¿ÀÛ È¯°æ »çÀÌÀÇ Á¾¼Ó¼ºÀ» Á¦°ÅÇÒ ÇÊ¿ä°¡ ÀÖÀ¸¸ç, ÀÌ´Â ºñÇà ¼ÒÇÁÆ®¿þ¾îÀÇ À̽ļº Çâ»óÀ» ÅëÇØ ´Þ¼ºÇÒ ¼ö ÀÖ´Ù. º» ³í¹®¿¡¼­´Â À̸¦ À§ÇØ IMA ¾ÆÅ°ÅØó ±â¹ÝÀÇ Ç÷§Æû ¾ÆÅ°ÅØó¸¦ Á¦¾ÈÇÑ´Ù. ÀÌ ¾ÆÅ°ÅØó´Â À̽ļºÀ» ±Ø´ëÈ­Çϱâ À§ÇØ µÎ °¡ÁöÀÇ IMA ¾ÆÅ°ÅØó ½ÇÇö ¹æ¾ÈÀ» ±â¹ÝÀ¸·Î ±¸ÃàµÈ È¥ÇÕÇü ¾ÆÅ°ÅØóÀÌ´Ù. ¶ÇÇÑ È¥ÇÕÇü ¾ÆÅ°ÅØóÀÇ °ËÁõÀ» À§ÇØ È¥ÇÕÇü ¾ÆÅ°ÅØó ±â¹ÝÀÇ ½Ã½ºÅÛÀ» ±¸ÇöÇÏ°í µ¿ÀÛ °á°ú¸¦ ºÐ¼®ÇÑ´Ù. º» ³í¹®¿¡¼­ Á¦¾ÈÇÑ ¾ÆÅ°ÅØó¸¦ ÅëÇؼ­ ºñÇà ¼ÒÇÁÆ®¿þ¾î¿Í µ¿Á÷ ȯ°æ »çÀÌÀÇ Á¾¼Ó¼ºÀ» Á¦°ÅÇÒ ¼ö ÀÖ´Ù.G¸ÁÀ» È°¿ëÇÏ¿© ²÷±è¾ø´Â ¼­ºñ½º¸¦ Áö¿øÇÒ ¼ö ÀÖ´Â ¹æ¾ÈÀ» Á¦¾ÈÇÏ¿´À¸¸ç, Å×½ºÆ®º£µå ±¸ÇöÀ» ÅëÇÏ¿© Á¦¾È ¹æ¾ÈÀÇ ¿ì¼ö¼ºÀ» °ËÁõÇÏ¿´´Ù.
¿µ¹®³»¿ë
(English Abstract)
Flight software operated on the on-board computers in the satellite has requirements such as real-time and high reliability. These requirements make dependency between the flight software and operating environments. Further, whenever a new system is built, such problem drives that all flight software are redeveloped. Thus, the dependency between them should be removed. And the work can be achieved by improving the portability of the flight software. In this paper, we propose a platform architecture based on the IMA architecture. The platform architecture is a hybrid one built by blending two kinds of realizations of the IMA architecture in order to maximize portability. In addition, we implement a prototype system and analyze the execution results of the system to justify the proposed architecture. The proposed architecture enables us to remove the dependency between fight software and operating environments.
Å°¿öµå(Keyword) ºñÇà ¼ÒÇÁÆ®¿þ¾î   ¼ÒÇÁÆ®¿þ¾î ¾ÆÅ°ÅØó   À̽ļº   Flight Software   Software Architecture   Portability  
ÆÄÀÏ÷ºÎ PDF ´Ù¿î·Îµå