The present invention relates to a landing reception apparatus for the landing of an aircraft and a control method thereof. According to the present invention, the landing reception apparatus comprises: a flight management system (FMS) receiving information on a scheduled landing airport, information on a scheduled landing runway and a receiver mode from a user; a data storage part storing final approach segment data for landing of an aircraft; a reception part calculating position information of the aircraft using a global navigation satellite system (GNSS) signal and a satellite-based augmentation systems (SBAS) signal transmitted from an antenna part when the input receiver mode is a GNSS/SBAS integrated mode; and an induced landing information generation part generating induced landing information using the final approach segment data corresponding to the input information on the scheduled landing airport and information on the scheduled landing runway and aircraft position information and transmitting the generated induced landing information to the FMS.

    본 발명은, 항공기 착륙을 위한 착륙 수신 장치 및 그 제어 방법에 관한 것으로, 본 발명에 따른 착륙 수신 장치는 사용자로부터 착륙 예정 공항, 착륙 예정 활주로 및 수신기 모드를 입력받는 FMS, 항공기의 착륙을 위한 최종접근경로 데이터를 저장하는 데이터 저장부, 입력된 수신기 모드가 GNSS/SBAS 통합 모드인 경우, 안테나부로부터 전송된 GNSS 신호와 SBAS 신호를 이용하여 항공기 위치 정보를 계산하는 수신기부, 그리고 입력된 착륙 예정 공항 및 착륙 예정 활주로에 대응하는 최종접근경로 데이터와 항공기 위치 정보를 이용하여 착륙 유도 정보를 생성하고, 생성된 착륙 유도 정보를 FMS에 전달하는 착륙 유도 정보 생성부를 포함한다.


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    Title :

    Aircraft Landing Apparatus Using GNSS and SBAS Singals and Control Method Thereof


    Additional title:

    위성 항법 신호를 이용한 항공기 착륙 수신 장치 및 그 제어 방법


    Publication date :

    2017-05-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Korean


    Classification :

    IPC:    G08G Anlagen zur Steuerung, Regelung oder Überwachung des Verkehrs , TRAFFIC CONTROL SYSTEMS / G01S RADIO DIRECTION-FINDING , Funkpeilung



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