운용 시스템(10)은, 접속선(13)과, 접속선(13)에 장력을 작용시키는 권취 장치(14)와, 접속선(13)의 조출량을 검출하는 조출량 검출부(34)와, 접속선(13)의 피검출부(13a)에 작용하는 힘의 방향을 검출하는 방향 검출부(35)와, 무인항공기(20)의 위치를 판정하는 위치 판정부(52)를 구비하고, 위치 판정부(52)는, 조출량 검출부(34)의 검출 결과에 기초하여 미리 정해진 기준 위치로부터 무인항공기(20)까지의 거리를 판정하고, 방향 검출부(35)의 검출 결과에 기초하여 피검출부(13a)를 기준으로 한 무인항공기(20)의 방위를 판정한다.
An operation system includes: a connecting cable; a winder configured to cause a tensile force to act on the connecting cable; a delivered amount detecting section configured to detect the delivered amount of the connecting cable; a direction detecting section configured to detect a direction of a force acting on a to-be-detected part of the connecting cable; and a position determination section configured to determine a position of an unmanned aircraft. The position determination section determines a distance from a predetermined reference position to the unmanned aircraft based on a detection result from the delivered amount detecting section. The position determination section determines an orientation of the unmanned aircraft on the basis of the to-be-detected part based on a detection result from the direction detecting section.
OPERATION SYSTEM OF UNMANNED AIRCRAFT
무인항공기의 운용 시스템
2024-03-14
Patent
Electronic Resource
Korean
IPC: | G05D SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES , Systeme zum Steuern oder Regeln nichtelektrischer veränderlicher Größen / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen / B64U |
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