$\require{mediawiki-texvc}$
  • 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

Method, apparatus and computer program product for estimating airplane attitude with reduced sensor set

국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판) G05D-001/00   
미국특허분류(USC) 701/004; 701/003; 701/007; 244/1580R; 244/171; 340/967
출원번호 US-0746316 (2000-12-22)
발명자 / 주소
출원인 / 주소
인용정보 피인용 횟수 : 23  인용 특허 : 2
초록

An apparatus, method and computer program product useful for supplying the pilot of an aircraft with aircraft attitude information in the event of full or partial failure of the gyroscopic system normally used to supply such data. The pitch angle, roll angle and heading angle estimates provided by the apparatus, method and computer program product can be displayed to the pilot thereby alleviating the requirement that the pilot mentally integrate such data from the remaining aircraft instruments.

대표
청구항

1. A system for supplying the pilot of an aircraft with an alternative source of aircraft attitude information comprising:a plurality of sensors including: a first sensor useful for sensing aircraft linear acceleration in a vertical direction; a second sensor useful for sensing an airspeed of the aircraft; a third sensor useful for sensing a roll rate and yaw rate of the aircraft and oriented on an inclined axis; a fourth sensor useful for sensing a magnetic heading of the aircraft; a signal processor, having an input coupled to said suite of sensors, an...

이 특허를 인용한 특허 피인용횟수: 23

  1. Kane,Richard L.. Aircraft pilot assistance system and method. USP2007107286911.
  2. Johnson, Jeffrey L.; Butts, Nicholas L.. Automatic multi-generational data caching and recovery. USP2015109172481.
  3. Le Texier, Maxime; Duchams, Georges. Device to aid the positioning of a pilot in an aircraft. USP2010067733480.
  4. Weinmann, Robert Vincent; Batcheller, Barry Douglas; Ohlsen, Tyler Chris; Halvorson, Jacob Andrew; Schubert, Seth Jamin. Fleet operations quality management system. USP2013108565943.
  5. Weinmann, Robert V.; Batcheller, Barry D.; Ohlsen, Tyler C.; Halvorson, Jacob A.; Johnson, Jeffrey L.; Butts, Nicholas L.; Schubert, Seth J.. Fleet operations quality management system and automatic multi-generational data caching and recovery. USP2015069047717.
  6. Batcheller, Barry Douglas; Ohlsen, Tyler Chris. Flight training and synthetic flight simulation system and method. USP2010127848698.
  7. Batcheller, Barry Douglas; Ohlsen, Tyler Chris. Flight training and synthetic visualization system and method. USP2012098265542.
  8. Clark,Becky L.; Ricco,Tina L.; Fay,Christopher W.. Graphical clinometer display system and method. USP2007127305772.
  9. Batcheller, David C.; Weinmann, Robert V.; Batcheller, Barry D.; Halvorson, Jacob A.; Johnson, Jeffrey L.; Butts, Nicholas L.; Tolstedt, Jonathan L.. Ground fleet operations quality management system. USP2015129202318.
  10. Shaw, Robert L.. Low cost flight instrumentation system. USP2015069057627.
  11. Perrie, Jean-Damien; Brivet, Valérie; Saint-Aroman, Stéphane. Method and device for automatically estimating an air speed of an aircraft. USP2013108552888.
  12. O'Neill, Kenneth Robert. Method and system for detecting errors in indicated air speed. USP2015099128109.
  13. Revol, Marc; Mandle, Jacques; Bibaut, Alain; Coatantiec, Jacques. Method and system for determining the attitude of an aircraft by multi-axis accelerometric measurements. USP2014028655511.
  14. Zaat, Stephen V.. Method and system for discovering and recovering unused service life. USP2003096618654.
  15. Tzidon, Aviv. Method for aircraft position prediction based on aircraft characteristics. USP2010117835866.
  16. Price,Ricardo A.. Method for determining roll rate gyro bias in an attitude heading reference system. USP2008097430460.
  17. Bensch, Lars; Henrichfreise, Hermann; Jusseit, Juergen; Merz, Ludger. Method for reconstructing gusts and structural loads at aircraft, in particular passenger aircraft. USP2012068209159.
  18. Fitzpatrick, David. Performing corrective action on unmanned aerial vehicle using one axis of three-axis magnetometer. USP2013028386095.
  19. Feyereisen, Thea L.. Pictographic mode awareness display for aircraft. USP2005056892118.
  20. Gelinske, Joshua N.; Allen, Robert M.; Batcheller, Barry D.; Halvorson, Jacob A.; Ohlsen, Tyler C.; Schubert, Seth J.; Weinmann, Robert V.; Wiig, Johan A.. Synchronized video and synthetic visualization system and method. USP2015028944822.
  21. Fouche, J. Michael. System and method for controlling model aircraft. USP2004066751529.
  22. Hausmann, Wolfgang. System of pitch attitude symbols. USP2004026686850.
  23. Manfred, Mark T.; Ryno, Thomas A.. Systems and methods of redundancy for aircraft inertial signal data. USP2012068204635.