검색연산자 | 기능 | 검색시 예 |
---|---|---|
() | 우선순위가 가장 높은 연산자 | 예1) (나노 (기계 | machine)) |
공백 | 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 | 예1) (나노 기계) 예2) 나노 장영실 |
| | 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 | 예1) (줄기세포 | 면역) 예2) 줄기세포 | 장영실 |
! | NOT 이후에 있는 검색어가 포함된 문서는 제외 | 예1) (황금 !백금) 예2) !image |
* | 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 | 예) semi* |
"" | 따옴표 내의 구문과 완전히 일치하는 문서만 검색 | 예) "Transform and Quantization" |
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.
NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) | F41G-005/18 |
미국특허분류(USC) | 89/4121 ; 89/4105 ; 356/252 ; 364/423 |
출원번호 | US-0425392 (1982-09-28) |
우선권정보 | FR-0019344 (1981-10-14) |
발명자 / 주소 |
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출원인 / 주소 |
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인용정보 | 피인용 횟수 : 12 인용 특허 : 7 |
Firing control system for a direct firing weapon mounted on a rotary-wing aircraft, which is designed to be actuated by the pilot himself and comprises an electronic computer, the said weapon being mounted for rotating about two transverse axes Y-Y′and Z-Z′, due to driving means controlled by the said computer. According to the invention, said firing control system is characterized in that it comprises a sighting system on which a target and an adjusting mark can appear simultaneously, which adjusting mark can be moved on the said sighting system by a co...
Firing control system for a weapon mounted on an aircraft and firing a projectile which travels in essentially a straight line, said system comprising: an electronic computer; mounting means for mounting said weapon on said aircraft for rotation about two transverse axes; driving means controlled by said computer for rotating said weapon about said axes; optical sighting means providing a field of view which is fixed relative to said axes and which permits a direct line-of-sight to a target by a pilot of said aircraft; an electro-optical device generatin...