LEADER 01892nam  2200337   450 
001 9910440243103321
005 20231209100048.0
010   $a1-5044-7098-2
024 7 $a10.1109/IEEESTD.2021.9354136
035   $a(CKB)4100000011763370
035   $a(NjHacI)994100000011763370
035   $a(EXLCZ)994100000011763370
100   $a20231209d2021      uy             0
101 0 $aeng
135   $aur|||||||||||
181   $ctxt$2rdacontent
182   $cc$2rdamedia
183   $acr$2rdacarrier
200 10$a1937.1-2020 $eIeee standard interface requirements and performance characteristics of payload devices in drones /$fInstitute of Electrical and Electronics Engineers
210  1$aNew York, New York :$cIEEE,$d2021.
215   $a1 online resource (30 pages)
330   $aGeneral interface requirements and performance characteristics of payload devices in drones are presented. The drone payload interfaces are described in three categories: mechanical interface, electrical interface, and data interface. Mechanical interface is used to fix the payload to the drone. Electrical interface is an electromechanical device used to join electrical terminations. The electrical interface includes the power supply interface and the two-way communication interface. Data interface refers to the communication protocol. The requirements and performance characteristics of the drone payload interface are detailed from the aspect of protection from temperature extremes, humidity, water, dust, vibration/shock, mold, salt spray, etc. Typical drone payloads, interface requirements, and performance characteristics of specific payloads are illustrated.
606   $aDrone aircraft
615  0$aDrone aircraft.
676   $a623.7469
801  0$bNjHacI
801  1$bNjHacl
906   $aDOCUMENT
912   $a9910440243103321
996   $a1937.1-2020$93654390
997   $aUNINA