CANNON LAUNCHED GUIDED PROJECTILE AND RF DIRECTION FINDER THEREFOR

The present invention relates to a guided aerial vehicle for an artillery, comprising: a flying projectile; a radome formed in a streamlined shape at the tip of the flying projectile; a navigation guidance control device mounted in the radome to control the guided flight of the flying projectile; an...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: CHOI JAE HYUN, JANG JONG HUN, KIM JIN SEOK, BANG JAE WON
Format: Patent
Sprache:eng ; kor
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Beschreibung
Zusammenfassung:The present invention relates to a guided aerial vehicle for an artillery, comprising: a flying projectile; a radome formed in a streamlined shape at the tip of the flying projectile; a navigation guidance control device mounted in the radome to control the guided flight of the flying projectile; and a radio frequency direction finder mounted in the radome, and receiving an RF signal to track the position of a GPS jammer, thereby capable of enabling the guided flight by precisely tracking the GPS jammer target. 본 발명은 비행 탄체, 상기 비행 탄체의 선단부에 유선형으로 형성되는 레이돔, 상기 레이돔 내에 탑재되어, 상기 비행 탄체의 유도 비행을 제어하는 항법 유도 제어 장치 및 상기 레이돔 내에 탑재되어, RF 신호를 수신하여 GPS 재머(GPS jammer)의 위치를 추적하기 위한 무선 주파수 방향 탐색기를 포함하는 화포용 유도 비행체로서, 본 발명에 의하면, GPS 재머 표적을 정밀 추적하여 유도 비행 가능하게 한다.