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Ç¥ÁعøÈ£ | TTAK.KO-11.0235-Part1 | ±¸Ç¥ÁعøÈ£ | |
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Á¦°³Á¤ÀÏ | 2017-12-13 | ÃÑÆäÀÌÁö | 16 |
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¿µ¹®Ç¥Áظí | UAV Battery Management System ? Part1: Battery Design Requirements | ||
Çѱ۳»¿ë¿ä¾à | ¹«Àε¿·Â ºñÇàÀåÄ¡¿ë ¹èÅ͸®ÀÇ Àû¿ë ´ë»óÀÌ ºñÇàÇÏ´Â ¹°Ã¼¶ó´Â Á¡¿¡¼ µ¿·Â¿øÀÎ ¹èÅ͸®ÀÇ °íÀåÀº Ã߶ôÀ¸·Î ÀÎÇÑ ÇÇÇػӸ¸ ¾Æ´Ï¶ó ½É°¢ÇÑ 2Â÷ ÇÇÇظ¦ ÀÏÀ¸Å³ ¼ö ÀÖ´Ù. µû¶ó¼ ¹èÅ͸®ÀÇ ½Å·Ú¼º°ú ¾ÈÁ¤¼ºÀ» È®º¸Çϱâ À§ÇÏ¿© Á¦ÀÛ ½Ã Àü±âÀû, ±â°èÀûÀÎ ¼³°è °í·Á»çÇ×À» ¼ö·ÏÇÏ°í ¼º´ÉÀ¯Áö¸¦ À§ÇÑ À¯Áö º¸¼ö ¹æ¹ý ¹× ¹«Àε¿·Â ºñÇàÀåÄ¡¿¡ ¸Â´Â ¹èÅ͸® ¼±Á¤ °í·Á »çÇ×À» ¼ö·ÏÇÏ¿´´Ù | ||
¿µ¹®³»¿ë¿ä¾à | Since the unmanned aerodrome battery is a flying object, the failure of the battery, which is the power source, can cause serious secondary damage as well as damage caused by the fall. Therefore, in order to assure the reliability and stability of the battery, electrical and mechanical design considerations are included in the production, maintenance methods for performance maintenance, and battery selection considerations for unmanned power train devices are listed. | ||
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°ü·ÃÆÄÀÏ | TTAK.KO-11.0235-Part1.pdf |