MONOPULSE TRACKING METHOD AND SYSTEM BASED ON MULTI STATE MODE

According to an embodiment of the present invention, provided is a monopulse satellite tracking method based on a multi-state mode, which includes the steps of: receiving satellite signals from a satellite and multi-channel signals from an antenna by an antenna control panel; outputting an error ang...

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Bibliographische Detailangaben
Hauptverfasser:	LEE DONG HYEOK, KIM JAE SIN, NOH SUNG MIN
Format:	Patent
Sprache:	eng ; kor
Schlagworte:	ANALOGOUS ARRANGEMENTS USING OTHER WAVES ANTENNAS, i.e. RADIO AERIALS BASIC ELECTRIC ELEMENTS DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES ELECTRICITY LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION ORRERADIATION OF RADIO WAVES MEASURING PHYSICS RADIO DIRECTION-FINDING RADIO NAVIGATION TESTING
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Beschreibung
Zusammenfassung:	According to an embodiment of the present invention, provided is a monopulse satellite tracking method based on a multi-state mode, which includes the steps of: receiving satellite signals from a satellite and multi-channel signals from an antenna by an antenna control panel; outputting an error angle based on the multi-channel signal by the antenna control panel; outputting a beam angle of the antenna by performing a transition algorithm for switching between a plurality of individual modes based on the satellite signal and the multi-channel signal by the antenna control panel; and controlling the driving of the antenna based on the beam angle by an antenna driving panel. Therefore, the continuity and stability of satellite tracking can be secured. 본 발명의 일 실시예에 따른 다중 상태 모드 기반의 모노펄스 위성 추적 방법은 안테나 제어반에 의해 위성으로부터 위성신호 및 안테나로부터 다채널 신호를 수신하는 단계; 상기 안테나 제어반에 의해 상기 다채널 신호를 기초로 오차각을 출력하는 단계; 상기 안테나 제어반에 의해 상기 위성신호 및 상기 다채널 신호를 기초로 복수의 개별 모드들 간의 전환을 수행하는 천이 알고리즘을 수행하여 안테나의 지향각을 출력하는 단계; 및 안테나 구동반에 의해 상기 지향각을 기초로 안테나의 구동을 제어하는 단계;를 포함한다.