JP4447791B2 - ジャイロメータと加速度計を具備する航空機の姿勢決定装置 - Google Patents

ジャイロメータと加速度計を具備する航空機の姿勢決定装置 Download PDF

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JP4447791B2
JP4447791B2 JP2000597607A JP2000597607A JP4447791B2 JP 4447791 B2 JP4447791 B2 JP 4447791B2 JP 2000597607 A JP2000597607 A JP 2000597607A JP 2000597607 A JP2000597607 A JP 2000597607A JP 4447791 B2 JP4447791 B2 JP 4447791B2
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vector
correction
gyro
aircraft
vertical
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JP2002538033A5 (enExample
JP2002538033A (ja
Inventor
ニコラス マルタン，
ジャン−ルネ シュヴァリエ，
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タレス アヴィオニックス エス．アー．
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    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/183—Compensation of inertial measurements, e.g. for temperature effects
    • G01C21/188—Compensation of inertial measurements, e.g. for temperature effects for accumulated errors, e.g. by coupling inertial systems with absolute positioning systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/10—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration
    • G01C21/12—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning
    • G01C21/16—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by using measurements of speed or acceleration executed aboard the object being navigated; Dead reckoning by integrating acceleration or speed, i.e. inertial navigation
    • G01C21/183—Compensation of inertial measurements, e.g. for temperature effects
    • G01C21/185—Compensation of inertial measurements, e.g. for temperature effects for gravity

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  • Engineering & Computer Science (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Navigation (AREA)
  • Gyroscopes (AREA)
JP2000597607A 1999-02-02 2000-01-31 ジャイロメータと加速度計を具備する航空機の姿勢決定装置 Expired - Fee Related JP4447791B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR99/01181 1999-02-02
FR9901181A FR2789172B1 (fr) 1999-02-02 1999-02-02 Appareil a gyrometres et accelerometres pour la determination des attitudes d'un aerodyne
PCT/FR2000/000219 WO2000046573A1 (fr) 1999-02-02 2000-01-31 Appareil a gyrometres et accelerometres pour la determination des attitudes d'un aerodyne

Publications (3)

Publication Number Publication Date
JP2002538033A JP2002538033A (ja) 2002-11-12
JP2002538033A5 JP2002538033A5 (enExample) 2009-07-30
JP4447791B2 true JP4447791B2 (ja) 2010-04-07

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ID=9541507

Family Applications (1)

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JP2000597607A Expired - Fee Related JP4447791B2 (ja) 1999-02-02 2000-01-31 ジャイロメータと加速度計を具備する航空機の姿勢決定装置

Country Status (8)

Country Link
US (1) US6588117B1 (enExample)
EP (1) EP1157254B1 (enExample)
JP (1) JP4447791B2 (enExample)
BR (1) BR0007735A (enExample)
CA (1) CA2361727A1 (enExample)
DE (1) DE60018719T2 (enExample)
FR (1) FR2789172B1 (enExample)
WO (1) WO2000046573A1 (enExample)

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* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10115217C1 (de) * 2001-03-28 2002-08-14 Bosch Gmbh Robert Verfahren zum Bestimmen der Winkellage eines Fahrzeugs
FR2833714B1 (fr) * 2001-12-18 2004-04-02 Thales Sa Procede de traitement d'un signal de navigation contenant des donnees
FR2834144B1 (fr) * 2001-12-20 2004-02-27 Thales Sa Convertisseur et convertisseur inverse (moyenne, ecart), correcteur de boucle, recepteur et procede de reception bi-frequence associe les utilisant
FR2837638B1 (fr) * 2002-03-22 2006-07-14 Thales Sa Procede de traitement de signal en presence d'interferences
FR2841069B1 (fr) * 2002-06-14 2004-10-22 Thales Sa Recepteur de positionnement par satellite utilisant deux porteuses de signal
FR2843638B1 (fr) * 2002-08-13 2004-10-22 Thales Sa Recepteur de positionnement par satellite avec correction d'erreurs d'inter-correlation
RU2249791C2 (ru) * 2003-06-24 2005-04-10 Федеральное государственное унитарное предприятие "Конструкторское бюро "Луч" Бесплатформенная инерциальная курсовертикаль
FR2869997B1 (fr) * 2004-05-04 2006-06-23 Commissariat Energie Atomique Accelerometre en boucle fermee avec detection d'erreur
FR2871313B1 (fr) * 2004-06-08 2006-08-18 Thales Sa Procede de transmission d'un signal de radionavigation
FR2895073B1 (fr) * 2005-12-20 2008-02-08 Thales Sa Dispositif d'hybridation en boucle fermee avec surveillance de l'integrite des mesures.
KR100711261B1 (ko) * 2006-06-21 2007-04-25 (주)마이크로인피니티 입력 장치의 공간 인식 방법 및 그 장치
WO2008033870A2 (en) 2006-09-11 2008-03-20 Lumexis Corporation Fiber-to-the-seat (ftts) fiber distribution system
RU2337316C1 (ru) * 2006-12-11 2008-10-27 Российская Федерация, от имени которой выступает государственный заказчик Министерство обороны Российской Федерации Бесплатформенная инерциальная система
SE531778C2 (sv) * 2007-01-09 2009-08-04 C2Sat Comm Ab Förfarande för att driftkompensera ett positionsmätningsorgan
US8326561B2 (en) * 2008-05-20 2012-12-04 Airmar Technology Corporation Dynamic motion control
EP2462513B1 (en) 2009-08-06 2018-12-19 Global Eagle Entertainment Inc. Serial networking fiber-to-the-seat inflight entertainment system
WO2011020071A1 (en) 2009-08-14 2011-02-17 Lumexis Corp. Video display unit docking assembly for fiber-to-the-screen inflight entertainment system
WO2011022708A1 (en) 2009-08-20 2011-02-24 Lumexis Corp. Serial networking fiber optic inflight entertainment system network configuration
US9383384B2 (en) * 2013-05-31 2016-07-05 Honeywell International Inc. Extended-range closed-loop accelerometer
US20220234700A1 (en) * 2019-08-16 2022-07-28 WP Controls, LLC Boat lift systems and methods

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3597598A (en) * 1964-12-14 1971-08-03 North American Rockwell Method and means for transforming the acceleration signals generated by accelerometers in a first coordinate system into acceleration signals in a second coordinate system
US3974699A (en) * 1973-08-28 1976-08-17 Systron Donner Corporation Angular position sensing and control system, apparatus and method
US4070674A (en) * 1973-10-17 1978-01-24 The Singer Company Doppler heading attitude reference system
US3979090A (en) * 1975-03-17 1976-09-07 Sperry Rand Corporation Velocity damped erection system for stable gyroscopic attitude and heading reference apparatus
US4179818A (en) * 1976-10-07 1979-12-25 Litton Systems, Inc. Tetrahedral redundant inertial reference unit
FR2511146B1 (fr) * 1981-08-07 1986-07-25 British Aerospace Instrument de navigation
DE3634023A1 (de) * 1986-10-07 1988-04-21 Bodenseewerk Geraetetech Integriertes, redundantes referenzsystem fuer die flugregelung und zur erzeugung von kurs- und lageinformationen
US5297052A (en) * 1989-10-16 1994-03-22 The Boeing Company Integrated fault-tolerant air data inertial reference system
US5479161A (en) * 1994-03-25 1995-12-26 Honeywell Inc. Automatic calibration of redundant sensors

Also Published As

Publication number Publication date
US6588117B1 (en) 2003-07-08
FR2789172B1 (fr) 2001-04-13
WO2000046573A1 (fr) 2000-08-10
BR0007735A (pt) 2002-01-29
CA2361727A1 (fr) 2000-08-10
DE60018719T2 (de) 2006-04-13
DE60018719D1 (de) 2005-04-21
EP1157254B1 (fr) 2005-03-16
EP1157254A1 (fr) 2001-11-28
FR2789172A1 (fr) 2000-08-04
JP2002538033A (ja) 2002-11-12

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