• 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
  • 검색연산자
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"

특허 상세정보

Apparatus for guiding a missile

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) F41G-007/26   
미국특허분류(USC) 244/313
출원번호 US-0005697 (1987-01-22)
우선권정보 CH-0000349 (1986-01-30)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 10  인용 특허 : 8

The apparatus for guiding a missile generates an electromagnetic guide beam such as a CO2-laser guide beam including spatial coding. For spatially encoding the guide beam there is employed a modulator as well as a scanning device which are intercoupled by means of a computer. The guide beam is moved in steps or increments by the scanning device in order to scan individual field sectors of a scanning field. Following each individual step, a code is transferred to or associated with a scanned field sector of the scanning field by the guide beam such that f...


An apparatus for guiding a missile, comprising: means for generating an electromagnetic guide beam guiding the missile along a trajectory leading to a target; encoding means for encoding in said guide beam generated by said guide beam generating means, data required for guiding said missile along the trajectory leading to the target; deflecting means for incrementally deflecting said encoded guide beam through a predetermined number of field sectors of a predetermined scanning field; a computer; and said encoding means and said deflecting means being mut...

이 특허를 인용한 특허 피인용횟수: 10

  1. Wolff Hendrikus J. (Hengelo NLX) Haverdings Hendrik (Borne NLX) Zwart Hendrik J. (Hengelo NLX). Course-correction system for course-correctable objects. USP1991034997144.
  2. Romer Rudolf (Kaarst DEX) Wollmann Gerd (Oberhausen DEX) Misoph Helmut (Lauf a.d. Pegnitz DEX). Method and apparatus for flight path correction of projectiles. USP1997025601255.
  3. Seidensticker, Jens. Method for correcting the trajectory of a projectile, in particular of a terminal phase-guided projectile, and projectile for carrying out the method. USP2013108558151.
  4. Weiss, Martin; Ruizenaar, Marcel Gregorius Anthonius. Method of guiding a salvo of guided projectiles to a target, a system and a computer program product. USP2014068748787.
  5. Feldmann, Michael Steven; Saggio, III, Frank; Washburn, John Robert. Methods for adjusting a relative navigation system. USP2014108872081.
  6. Yu, Wai. Missile guidance. USP2015049012822.
  7. Glaros, Louis N.; Eddins, William B.; Gaylord, Charles; Kincheloe, Michael. Spot leading target laser guidance for engaging moving targets. USP2012088237095.
  8. Buehler, Eric Daniel; McCauley, David Kevin. System and method for utilizing multiple sensors. USP2016049322651.
  9. Feldmann, Michael Steven; Saggio, III, Frank; Paasche, Timothy John; Turner, Mark Lawrence; Ingersoll, John Andrew. System and methods of detecting an intruding object in a relative navigation system. USP2016099435635.
  10. Arnaud Philippe (Orleans La Source FRX) Bernard Marc (Marcilly en Villette FRX). System for carrier guidance by laser beam and pyrotechnic thrusters. USP1990024901946.