LANDING SYSTEM FOR AIRFLIGHT

• Main Authors: LEE SU JIN, LEE MIN SEOK, YOU DONG IL, LIM HEUNG SIK
• Format: Patent
• Language: English; Korean
• Published: 03.07.2023
• Subjects: AEROPLANES; AIRCRAFT; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT; AVIATION; CALCULATING; COMPUTER SYSTEMS BASED ON SPECIFIC COMPUTATIONAL MODELS; COMPUTING; COSMONAUTICS; COUNTING; EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SUITS; HELICOPTERS; IMAGE DATA PROCESSING OR GENERATION, IN GENERAL; MEASURING; METEOROLOGY; PARACHUTES; PERFORMING OPERATIONS; PHYSICS; TESTING; TRANSPORTING

One embodiment of the present invention is to provide an aircraft landing system that can measure the wind at the landing site through image information from a wind measurement device at the landing site and allows an aircraft to safely land on the landing site through precise control based on the wind conditions at the landing site. According to one embodiment of the present invention, an aircraft landing system comprises: a first camera mounted on an aircraft and collecting first image information of the landing site; and an image information processing device which receives the first image information. The image information processing device may analyze the weather conditions of the landing site based on the first image information and transmit the analysis result to the aircraft. 일 실시 예에 따른 비행체 착륙 시스템은, 비행체에 탑재되어 착륙장의 제 1 영상 정보를 수집하는 제 1 카메라; 및 상기 제 1 영상 정보를 전달받는 영상 정보 처리 장치를 포함하고, 상기 영상 정보 처리 장치는, 상기 제 1 영상 정보를 기반으로 상기 착륙장의 기상 상태를 분석하고, 상기 비행체에 분석 결과를 전달할 수 있다.