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Apparatus and method for navigation of an aircraft

IPC분류정보
국가/구분 United States(US) Patent 등록
국제특허분류(IPC7판)
  • G01S-005/02
  • H04B-007/185
출원번호 US-0037401 (2002-01-04)
발명자 / 주소
  • McIntyre, Melville Duncan W.
출원인 / 주소
  • The Boeing Company
대리인 / 주소
    Alston & Bird LLP
인용정보 피인용 횟수 : 23  인용 특허 : 12

초록

In accordance with this invention, an apparatus and method for aircraft navigation are provided that utilize a blended architecture consisting of a global positioning system (GPS) and micro-electromechanical sensors (MEMS) for the primary navigation system and a laser gyroscope system for the second

대표청구항

In accordance with this invention, an apparatus and method for aircraft navigation are provided that utilize a blended architecture consisting of a global positioning system (GPS) and micro-electromechanical sensors (MEMS) for the primary navigation system and a laser gyroscope system for the second

이 특허에 인용된 특허 (12)

  1. Sheikh Suneel I. ; Vallot Lawrence C. ; Schipper Brian W., Attitude determination method and system.
  2. Lin Ching-Fang, Enhanced integrated positioning method and system thereof for vehicle.
  3. McClary Charles R., Fault tolerant inertial reference system.
  4. Ching-Fang Lin, Fully-coupled positioning process and system thereof.
  5. Divakaruni Sudhakar P., GPS/IRS global position determination method and apparatus with integrity loss provisions.
  6. Ebner Robert E. (Auburn CA) Brown Ronald A. (Seminole FL), Integrated GPS/inertial navigation apparatus providing improved heading estimates.
  7. Bruckner Juergen M. ; Hwang Patrick Y., Method and apparatus for achieving sole means navigation from global navigation satelite systems.
  8. Mickelson Wilmer A., Navigation system for spinning projectiles.
  9. Ching-Fang Lin, Positioning and proximity warning method and system thereof for vehicle.
  10. Ignagni Mario B. (Arden Hills MN), True north heading estimator utilizing GPS output information and inertial sensor system output information.
  11. Lin Ching-Fang, Vehicle positioning method and system thereof.
  12. Lin Ching-Fang, Vehicle positioning method and system thereof.

이 특허를 인용한 특허 (23)

  1. Einig, Johannes; Gross, Claus-Peter, Control device, input/output device, connection switch device and method for an aircraft control system.
  2. Einig, Johannes; Gross, Claus-Peter, Control device, input/output device, connection switch device and method for an aircraft control system.
  3. Pedrazzini,Giorgio; Lasalandra,Ernesto; Vigna,Bendetto, Electronic device including motion sensitive power switching integrated circuit and related methods.
  4. Paulsen, Lee M.; Michaels, Donald L.; Thompson, Robert J.; Cook, Michael J.; Mather, John C., Low profile, conformal global positioning system array for artillery.
  5. Linn, Eric H.; Deeds, Michael A.; Herman, David, MEMS type thermally actuated out-of-plane lever.
  6. Hall, Mark D.; Force, Timothy M., Method and system for establishing a system time within a mobile ad hoc network.
  7. Ishihara, Yasuo; Conner, Kevin J; Johnson, Steve C., Method of detecting erroneous GPS ground speed on ground.
  8. Wright, George L.; Wright, Mark A., Method, system, and apparatus of vehicle and fleet operator profile automation and deployment.
  9. McKendree,Thomas L.; Britigan,John D.; Habereder,Hans L., Munition with integrity gated go/no-go decision.
  10. McKendree,Thomas L.; Britigan,John D.; Habereder,Hans L., Munition with integrity gated go/no-go decision.
  11. Script, Michael H., Portable motion detector and alarm system and method.
  12. Script, Michael H., Portable motion detector and alarm system and method.
  13. Script, Michael H.; Script, Henry J., Portable motion detector and alarm system and method.
  14. Li, Rongsheng; Ghassemi, Kamran; Kelley, Clifford W., Software GNSS receiver for high-altitude spacecraft applications.
  15. Schmidt, R. Kyle, System and method for determining aircraft hard landing events from inertial and aircraft reference frame data.
  16. Schmidt, R. Kyle, System and method for determining aircraft hard landing events from inertial and aircraft reference frame data.
  17. Ahlbrecht, Mark A.; Ibis, Michael R.; Morrison, John R., System and method for isolating attitude failures in aircraft.
  18. Bharadwaj, Raj Mohan; Bageshwar, Vibhor L.; Kim, Kyusung, Systems and methods for determining inertial navigation system faults.
  19. Overstreet,Lisa M.; Fall,Robert H., Systems and methods for improved inertial navigation.
  20. Miller, Michael G.; Horner, Adam Ross, Systems and methods for producing two independent dissimilar attitude solutions, two independent dissimilar inertial solutions or both from one improved navigation device.
  21. Hedrick, Geoffrey S. M.; Askarpour, Shahram; Knopf, Markus, Upgraded flight management system and method of providing the same.
  22. Hedrick, Geoffrey S. M.; Askarpour, Shahram; Knopf, Markus, Upgraded flight management system and method of providing the same.
  23. Hedrick, Geoffrey S. M.; Askarpour, Shahram, Upgraded flight management system for autopilot control and method of providing the same.
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