In-flight Impact Angle Determination Apparatus for Biased Proportional Navigation Guidance Method thereof and Computer readable storage having the same method

In-flight Impact Angle Determination Apparatus for Biased Proportional Navigation Guidance Method thereof and Computer readable storage having the same method

The present invention relates to a flight vehicle navigation technique and, more specifically, relates to an in-flight target impact angle determination apparatus for biased proportional navigation guidance and a method thereof. According to the present invention, an in-flight target impact angle ge...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: KANG SEUNG HOON, HAN SANG SUL, JUNG SHIN WON
Format: Patent
Sprache:eng ; kor
Schlagworte:
AIMING
AMMUNITION
BLASTING
EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
HEATING
LIGHTING
MECHANICAL ENGINEERING
WEAPON SIGHTS
WEAPONS
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Beschreibung
Zusammenfassung:The present invention relates to a flight vehicle navigation technique and, more specifically, relates to an in-flight target impact angle determination apparatus for biased proportional navigation guidance and a method thereof. According to the present invention, an in-flight target impact angle generated by relative geometry changed in launching time and hitting time. 본 발명은 비행체 항법 기술에 관한 것으로서, 더 상세하게는 부가 비례 항법 유도에서의 비행중 목표 충돌각 결정 장치 및 방법에 대한 것이다. 본 발명에 따르면, 발사 시점과 타격 시점에 달라지는 상대기하에 의해 발생하는 비행중 목표 충돌각 결정이 가능하다.