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| Ç¥ÁØÁ¾·ù | Á¤º¸Åë½Å´ÜüǥÁØ(TTAS) | ||||||||||||||||
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| Ç¥ÁعøÈ£ | TTAK.KO-11.0234 | ±¸ Ç¥ÁعøÈ£ | |||||||||||||||
| Á¦°³Á¤ÀÏ | 2017-12-13 | ÃÑ ÆäÀÌÁö | 21 | ||||||||||||||
| ÇÑ±Û Ç¥Áظí | ¸ÖƼÄßÅÍÇü ¹«ÀÎÇ×°ø±âÀÇ ¼³°è¿ä±¸»çÇ× ¹× ºñÇ༺´É½ÃÇè | ||||||||||||||||
| ¿µ¹® Ç¥Áظí | Design Requirements and Flight Performance Test for Multicopter UAV | ||||||||||||||||
| ÇÑ±Û ³»¿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 | ||||||||||||||||
| °ü·Ã IPR È®¾à¼ | Á¢¼öµÈ IPR È®¾à¼ ¾øÀ½ | ||||||||||||||||
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