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Ç¥ÁعøÈ£ TTAK.KO-11.0234 ±¸Ç¥ÁعøÈ£
Á¦°³Á¤ÀÏ 2017-12-13 ÃÑÆäÀÌÁö 21
ÇѱÛÇ¥ÁØ¸í ¸ÖƼÄßÅÍÇü ¹«ÀÎÇ×°ø±âÀÇ ¼³°è¿ä±¸»çÇ× ¹× ºñÇ༺´É½ÃÇè
¿µ¹®Ç¥Áظí Design Requirements and Flight Performance Test for Multicopter UAV
Çѱ۳»¿ë¿ä¾à ÀÌ Ç¥ÁØÀº ¹«ÀÎÇ×°ø±â ½Ã½ºÅÛ(UAS, Unmanned Aircraft Systems)¡¯Áß¿¡¼­ ¹«ÀÎÇ×°ø±â(UAV, Unmanned Arial Vehicle) ÀÇ ÃÖ´ë ÀÌ·úÁß·®ÀÌ 25kg ÀÌÇÏÀÎ ¸ÖƼÄßÅÍÇü ¹«ÀÎÇ×°ø±âÀÇ Á¦Á¶¿¡ ÇÊ¿äÇÑ ¼³°è¿ä±¸»çÇ× ¹× ±âº» ¼º´É ¹× ½ÃÇè¿¡ ´ëÇÏ¿© ±â¼úÇÑ´Ù.
¿µ¹®³»¿ë¿ä¾à The standard describes the design requirements, basic performance and tests required for the manufacture of multi-copter type UAVs with a maximum take-off weight of 25kg or less of unmanned aerial vehicles among unmanned aerial vehicle systems
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°ü·ÃÆÄÀÏ TTAK.KO-11.0234.pdf TTAK.KO-11.0234.pdf            

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