[특허]Systems and methods for boresight adapters

The Boeing Company

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

검색도움말
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"

과학기술 지식인프라 ScienceON

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

특허 상세정보

MyON담기

내보내기 페이스북 공유 트위터 공유 카카오톡 공유

Systems and methods for boresight adapters

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F41G-011/00 F41G-001/54 F41G-001/00 F41G-007/24 F41G-007/20
미국특허분류(USC)	244/003.1; 244/003.11; 244/003.13; 089/001.1; 089/001.11; 250/491.1
출원번호	UP-0067568 (2005-02-25)
등록번호	US-7550697 (2009-07-01)
발명자 / 주소	Veselovsky, Jeffrey S. Zimmerle, Andrew R. Van De Laare, Dean
출원인 / 주소	The Boeing Company
인용정보	피인용 횟수 : 2 인용 특허 : 30

초록
▼

Boresighting systems and methods are disclosed. In one embodiment, an assembly adapted for boresighting a launch system includes first and second elongated members adapted to be coupled to the launch system. First and second alignment members are coupled to and extend between the first and second elongated members and are adapted to position the elongated members in a substantially aligned, spaced-apart relationship. A mirror assembly is coupled to each elongated member, the mirror assemblies being adapted to provide an average angular position resulting...

대표
청구항
▼

What is claimed is: 1. An assembly adapted for boresighting a launch system, comprising: a measurement system having a processor; first and second elongated members configured to be coupled to the launch system; first and second alignment members coupled to and extending between the first and second elongated members and configured to position the elongated members in a substantially aligned, spaced-apart relationship; and a mirror assembly coupled to each elongated member, the mirror assemblies being configured to provide input to the processor, the processor being configured to determine, based on the input, an average angular position resulting in a single corrector value for the launch system, wherein the single corrector value is provided to the launch system for boresighting the launch system. 2. The assembly of claim 1, wherein each of the first and second elongated members includes a substantially-cylindrical body having a plurality of interface locations configured to be coupled to the launch system. 3. The assembly of claim 2, wherein at least one interface location comprises an annular band having a relatively larger diameter than a diameter of an adjacent portion of the substantially-cylindrical body. 4. The assembly of claim 1, wherein each alignment member includes an enlarged end coupled to a first one of the elongated members and a cylindrical end coupled to another of the elongated members. 5. The assembly of claim 1, wherein each mirror assembly includes a first mirror facing a first direction that is substantially parallel with a longitudinal axis of its associated elongated member, and a second mirror facing a second direction that is not parallel with the longitudinal axis. 6. The assembly of claim 5, wherein the first direction intersects the second direction. 7. A missile launch system, comprising: a base configured to be coupled to a launch platform, the based having a plurality of attachment devices configured to be coupled to at least one missile; an adapter assembly for sighting the base, the adapter assembly including: a measurement system having a processor; first and second elongated members configured to be coupled to the attachment devices of the base; first and second alignment members coupled to and extending between the first and second elongated members and configured to position the elongated members in a substantially aligned, spaced-apart relationship; and a mirror assembly coupled to each elongated member, the mirror assemblies being configured to provide input to the processor, the processor being configured to determine, based on the input, an average angular position resulting in a single corrector value for the missile launch system, wherein the single corrector value is provided to the launch system for boresighting the launch system. 8. The system of claim 7, wherein each of the first and second elongated members includes a substantially-cylindrical body having a plurality of interface locations configured to be coupled to the launch system. 9. The system of claim 8, wherein at least one interface location comprises an annular band having a relatively larger diameter than a diameter of an adjacent portion of the substantially-cylindrical body. 10. The system of claim 7, wherein each alignment member includes an enlarged end coupled to a first one of the elongated members and a cylindrical end coupled to another of the elongated members. 11. The system of claim 7, wherein each mirror assembly includes a first mirror facing a first direction that is substantially parallel with a longitudinal axis of its associated elongated member, and a second mirror facing a second direction that is not parallel with the longitudinal axis. 12. The system of claim 11, wherein the first direction intersects the second direction. 13. A method of sighting a launch system, comprising: engaging a first tube member of an adapter assembly with the launch system; engaging a second tube member of the adapter assembly with the launch system; adjusting a first position of the first tube member relative to the second tube member; securing the first tube member into the first position with respect to the launch system; adjusting a second position of the second tube member relative to the first tube member; securing the second tube member into the second position with respect to the launch system; performing measurements of at least one of the first and second positions; determining a corrector value based on the measurements of the at least one of the first and second positions; and boresighting the launch system using the single corrector value. 14. The method of claim 13, wherein engaging a first tube member of an adapter assembly with the launch system includes engaging an upper tube member of an adapter assembly with the launch system. 15. The method of claim 13, wherein engaging a second tube member of an adapter assembly with the launch system includes engaging an lower tube member of an adapter assembly with the launch system. 16. The method of claim 13, wherein at least one of adjusting a first position of the first tube member and adjusting a second position of the second tube member includes adjusting a position of a one of the tube members so that an end portion projecting outwardly from the one of the tube members is positioned tangent to the other of the tube members. 17. The method of claim 13, wherein at least one of securing the first tube member and securing the second tube member includes securing a plurality of clamps of the launch system. 18. The method of claim 13, wherein performing measurements of at least one of the first and second positions includes performing measurements of both the first and second positions. 19. The method of claim 13, wherein performing measurements of at least one of the first and second positions includes performing measurements of at least one of an elevation value, an azimuth value, and a roll value. 20. The method of claim 13, wherein determining a corrector value based on the measurements of the at least one of the first and second positions includes at least one of averaging the measurements and comparing the measurements with a predetermined value to determine the corrector value.

이 특허에 인용된 특허 (30)

이 특허를 인용한 특허 피인용횟수: 2

이 특허와 함께 이용한 콘텐츠

IPC 상위 출원인

내보내기

상세정보
내보내기 구분	파일저장 인쇄 메일전송
구성항목	관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표IPC 관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 공고번호, 공고일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표출원인, 출원인국적, 출원인주소, 발명자, 발명자E, 발명자코드, 발명자주소, 발명자 우편번호, 발명자국적, 대표IPC, IPC코드, 요약, 미국특허분류, 대리인주소, 대리인코드, 대리인(한글), 대리인(영문), 국제공개일자, 국제공개번호, 국제출원일자, 국제출원번호, 우선권, 우선권주장일, 우선권국가, 우선권출원번호, 원출원일자, 원출원번호, 지정국, Citing Patents, Cited Patents
저장형식	Text(ASCII format) Excel format PIAS분석(.xls)
메일정보	받는사람 (필수) @ 보내는사람 (선택) @ 제목 내용 KISTI 검색결과 이메일 서비스
안내	> 총 건의 자료가 검색되었습니다. > 다운받으실 자료의 인덱스를 입력하세요. (1-10,000) > 검색결과의 순서대로 최대 10,000건 까지 다운로드가 가능합니다. > 데이타가 많을 경우 속도가 느려질 수 있습니다.(최대 2~3분 소요) > 다운로드 파일은 UTF-8 형태로 저장됩니다. 파일의 내용이 제대로 보이지 않을실 때는 웹브라우저 상단의 보기 -> 인코딩 -> 자동선택 여부를 확인하십시오 > ~ > Text(ASCII format) Excel format

과학기술 지식인프라 ScienceON

ScienceON Chatbot

연합인증

특허 상세정보

Systems and methods for boresight adapters

초록
▼

대표
청구항
▼

이 특허에 인용된 특허 (30)

이 특허를 인용한 특허 피인용횟수: 2

이 특허와 함께 이용한 콘텐츠

IPC 상위 출원인

과제정보

상세정보조회

원문조회

IPC 상세정보(version : 201201)

연구과제 성과물(0)

참여연구원의 다른 문헌(0)

처리중입니다.

잠시만 기다려주세요.

ScienceON Chatbot

연합인증

특허 상세정보

Systems and methods for boresight adapters

초록 ▼

대표청구항 ▼

이 특허에 인용된 특허 (30)

이 특허를 인용한 특허 피인용횟수: 2

이 특허와 함께 이용한 콘텐츠

IPC 상위 출원인

과제정보

상세정보조회

원문조회

IPC 상세정보(version : 201201)

연구과제 성과물(0)

참여연구원의 다른 문헌(0)

처리중입니다.

잠시만 기다려주세요.

초록
▼

대표
청구항
▼