[특허]System for guiding an aircraft to a reference point in low visibility conditions

Elbit Systems Ltd.

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

System for guiding an aircraft to a reference point in low visibility conditions

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	G08G-005/00 G08G-005/02
출원번호	US-0582526 (2011-03-03)
등록번호	US-10096254 (2018-10-09)
국제출원번호	PCT/IB2011/050902 (2011-03-03)
§371/§102 date	20130212 (20130212)
국제공개번호	WO2011/107956 (2011-09-09)
발명자 / 주소	Nauman, Ron Efrat, Ilan Hartuv, Roee Halifa, Eyal Klein, Ofer Makov, Hagay Galed, Eran
출원인 / 주소	Elbit Systems Ltd.
대리인 / 주소	Pearl Cohen Zedek Latzer Baratz LLP
인용정보	피인용 횟수 : 0 인용 특허 : 2

초록
▼

A method of visually guiding a pilot flying an aircraft using one or more conformal symbols whose position is dynamically updated throughout the guidance is provided herein. The method includes the following stages: determining a desired flight route of an aircraft, based on a user-selected maneuver; presenting to a pilot, on a display, at least one 3D visual symbol that is: (i) earth-space stabilized, and (ii) positioned along a future location along the desired route; computing an updated desired route based on repeatedly updated aircraft flight data t...

대표
청구항
▼

1. A method comprising: determining a desired flight route of an aircraft, based on a desired maneuver;presenting to a pilot, on a display, at least one 3D visual symbol that is positioned along a future desired location and orientation on the flight desired route and moves at a desired momentary speed and a desired orientation relative to the earth, wherein the desired momentary speed and the desired orientation are determined based on the desired maneuver;computing an updated desired route based on repeatedly updated environmental conditions and aircraft flight data that include at least one of: current location and current speed and orientation of the aircraft; andrepeating the presenting of the at least one 3D visual symbol with an updated desired position and an updated desired momentary speed and updated desired orientation,wherein movements of said 3D visual symbol resemble movements of another aircraft in an aircraft formation and wherein said 3D symbol serves as a dynamic point of reference for said pilot, resembling following a real lead aircraft in said aircraft formation. 2. The method according to claim 1, wherein the display is embedded within a helmet worn by the pilot, and wherein the at least one 3D visual symbol further conforms to a line of sight of the pilot. 3. The method according to claim 1, wherein the display is a head up display (HUD) or a head down display (HDD). 4. The method according to claim 1, wherein the at least one 3D visual symbol comprises two or more 3D symbols located with regards to the desired maneuver. 5. The method according to claim 1, wherein the at least one 3D visual symbol includes representing a 3D orientation thereof. 6. The method according to claim 1, wherein the maneuver is landing, wherein the desired route ends in a landing point. 7. The method according to claim 1, wherein the method further comprises presenting a virtual representation of a surrounding of a landing point. 8. The method according to claim 1, wherein the desired maneuver is following a terrain, wherein the desired route is computed to be within a specified safety distance from the terrain. 9. The method according to claim 1, further comprising obtaining dynamic information regarding at least one of: environmental conditions or obstacles along the desired route, wherein the computing of the updated desired route is further based on the dynamic information. 10. The method according to claim 1, wherein the presenting is carried out stereoscopically, to provide a 3D depth sense of the at least one 3D visual symbol. 11. The method according to claim 1, wherein the at least one 3D visual symbol changes its shape and/or color indicative of a change in at least one of: (i) environmental conditions along the desired route; (ii) predefined phases along the desired route; and (iii) a predefined threshold. 12. The method according to claim 1, wherein the at least one 3D visual symbol resembles a shape of an aircraft. 13. A system comprising: a flight route calculator configured to determine a desired flight route of an aircraft, based on a desired maneuver;a display configured to present to a pilot, on a display, at least one 3D visual symbol that is positioned in a future desired location and a desired orientation along the desired flight route and moves at a desired momentary speed and a desired orientation relative to the earth, wherein the desired momentary speed and the desired orientation are determined based on the desired maneuver; anda processing unit configured to compute an updated desired route based on repeatedly updated environmental conditions and aircraft flight data that include at least one of: current location and current speed and orientation of the aircraft,wherein the display is further configured to repeat the presenting of the at least one 3D visual symbol with an updated desired position and an updated desired momentary speed and updated desired orientation,wherein movements of said 3D visual symbol resemble movements of another aircraft in an aircraft formation and wherein said 3D symbol serves as a dynamic point of reference for said pilot, resembling following a real lead aircraft in said aircraft formation. 14. The system according to claim 13, wherein the display is embedded within a helmet worn by the pilot, and wherein the at least one 3D visual symbol further conforms to a line of sight of the pilot. 15. The system according to claim 13, wherein the display is a head up display (HUD) or a head down display (HDD). 16. The system according to claim 13, wherein the at least one 3D visual symbol comprises two or more 3D symbols located along the updated desired route. 17. The system according to claim 13, wherein the at least one 3D visual symbol includes representing a 3D orientation thereof. 18. The system according to claim 13, wherein the desired maneuver is landing, wherein the desired route ends in a landing point. 19. The system according to claim 13, wherein the display is further configured to present a virtual representation of a surrounding of a landing point. 20. The system according to claim 13, wherein the desired maneuver is following a terrain, wherein the desired route is computed to be within a specified safety distance from the terrain. 21. The system according to claim 13, further, wherein the processing unit is configured to compute the updated desired route further based on dynamically obtained information regarding at least one of: environmental conditions or obstacles along the desired route. 22. The system according to claim 13, wherein the display is stereoscopic, providing a 3D depth sense of the at least one 3D visual symbol. 23. The system according to claim 13, wherein the at least one 3D visual symbol changes its shape and/or color indicative of a change in at least one of: (i) environmental conditions along the desired route; (ii) predefined phases along the desired route; and (iii) a predefined threshold. 24. The system according to claim 13, wherein the at least one 3D visual symbol resembles a shape of an aircraft. 25. The system according to claim 13, wherein the display is further configured to present a visual indicator that changes its height dynamically, based on a current altitude of the aircraft.

이 특허에 인용된 특허 (2)

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

System for guiding an aircraft to a reference point in low visibility conditions

초록
▼

대표
청구항
▼

이 특허에 인용된 특허 (2)

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

System for guiding an aircraft to a reference point in low visibility conditions

초록 ▼

대표청구항 ▼

이 특허에 인용된 특허 (2)

IPC 상위 출원인

과제정보

상세정보조회

원문조회

IPC 상세정보(version : 201201)

연구과제 성과물(0)

참여연구원의 다른 문헌(0)

처리중입니다.

잠시만 기다려주세요.

초록
▼

대표
청구항
▼