CA2361727A1 - Appareil a gyrometres et accelerometres pour la determination des attitudes d'un aerodyne - Google Patents
Appareil a gyrometres et accelerometres pour la determination des attitudes d'un aerodyne Download PDFInfo
- Publication number
- CA2361727A1 CA2361727A1 CA002361727A CA2361727A CA2361727A1 CA 2361727 A1 CA2361727 A1 CA 2361727A1 CA 002361727 A CA002361727 A CA 002361727A CA 2361727 A CA2361727 A CA 2361727A CA 2361727 A1 CA2361727 A1 CA 2361727A1
- Authority
- CA
- Canada
- Prior art keywords
- vector
- aerodyne
- vertical direction
- gyrometric
- accelerometers
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Abandoned
Links
- 239000013598 vector Substances 0.000 claims abstract description 151
- 238000012937 correction Methods 0.000 claims abstract description 29
- 239000011159 matrix material Substances 0.000 claims abstract description 18
- 238000005259 measurement Methods 0.000 claims abstract description 8
- 230000005484 gravity Effects 0.000 claims description 10
- 230000000694 effects Effects 0.000 claims description 3
- 230000001133 acceleration Effects 0.000 description 20
- 238000010586 diagram Methods 0.000 description 11
- 230000010354 integration Effects 0.000 description 5
- RZVAJINKPMORJF-UHFFFAOYSA-N Acetaminophen Chemical group CC(=O)NC1=CC=C(O)C=C1 RZVAJINKPMORJF-UHFFFAOYSA-N 0.000 description 3
- 244000089409 Erythrina poeppigiana Species 0.000 description 1
- 235000009776 Rathbunia alamosensis Nutrition 0.000 description 1
- 230000004075 alteration Effects 0.000 description 1
- 230000003321 amplification Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000001514 detection method Methods 0.000 description 1
- 239000000284 extract Substances 0.000 description 1
- 230000010006 flight Effects 0.000 description 1
- 239000003550 marker Substances 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 238000003199 nucleic acid amplification method Methods 0.000 description 1
- 210000000056 organ Anatomy 0.000 description 1
- 238000011282 treatment Methods 0.000 description 1
- 230000001960 triggered effect Effects 0.000 description 1
- 238000011144 upstream manufacturing Methods 0.000 description 1
Classifications
-
- 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
Landscapes
- 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)
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 (1)
| Publication Number | Publication Date |
|---|---|
| CA2361727A1 true CA2361727A1 (fr) | 2000-08-10 |
Family
ID=9541507
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA002361727A Abandoned CA2361727A1 (fr) | 1999-02-02 | 2000-01-31 | Appareil a gyrometres et accelerometres pour la determination des attitudes d'un aerodyne |
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) |
Families Citing this family (20)
| 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)
| 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 |
-
1999
- 1999-02-02 FR FR9901181A patent/FR2789172B1/fr not_active Expired - Fee Related
-
2000
- 2000-01-31 EP EP00902695A patent/EP1157254B1/fr not_active Expired - Lifetime
- 2000-01-31 CA CA002361727A patent/CA2361727A1/fr not_active Abandoned
- 2000-01-31 BR BR0007735-6A patent/BR0007735A/pt not_active IP Right Cessation
- 2000-01-31 US US09/889,578 patent/US6588117B1/en not_active Expired - Fee Related
- 2000-01-31 WO PCT/FR2000/000219 patent/WO2000046573A1/fr not_active Ceased
- 2000-01-31 JP JP2000597607A patent/JP4447791B2/ja not_active Expired - Fee Related
- 2000-01-31 DE DE60018719T patent/DE60018719T2/de not_active Expired - Fee Related
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 |
| 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 |
| JP4447791B2 (ja) | 2010-04-07 |
| JP2002538033A (ja) | 2002-11-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CA2361727A1 (fr) | Appareil a gyrometres et accelerometres pour la determination des attitudes d'un aerodyne | |
| EP2400460B1 (fr) | Procédé d'évaluation de la vitesse horizontale d'un drone, notamment d'un drone apte au vol stationnaire autopiloté | |
| EP2831685A1 (fr) | Procede de pilotage d'un drone a voilure tournante a rotors multiples avec estimation et compensation du vent lateral et du biais des accelerometres. | |
| EP2048475B1 (fr) | Procédé de détermination de l'attitude, de la position et de la vitesse d'un engin mobile | |
| EP3076258B1 (fr) | Drone muni d'une caméra video à visée verticale compensée des rotations instantanées pour l'estimation des vitesses horizontales | |
| FR2511146A1 (fr) | Instrument de navigation | |
| FR3007841A1 (fr) | Procede de detection d'une panne d'au moins un capteur present sur un aeronef, mettant en oeuvre une boucle baro-inertielle et systeme associe | |
| FR2495313A1 (fr) | Circuit de calcul d'inclinaison longitudinale pour un aeronef | |
| FR3007840A1 (fr) | Procede de detection d'une panne d'au moins un capteur present sur un aeronef, mettant en oeuvre une boucle anemo-inertielle, et systeme associe | |
| EP1205732B1 (fr) | Centrale inertielle de navigation comportant un récepteur GPS intégré | |
| FR2670592A1 (fr) | Procede et systeme de securisation des informations de pilotage d'un aeronef. | |
| EP2694375A1 (fr) | Dispositif et procede de determination d'attitude d'un satellite, et satellite embarquant un tel dispositif | |
| FR2697651A1 (fr) | Procédé et appareil de calibration des gyromètres d'un satellite stabilisé 3-axes. | |
| EP3899432B1 (fr) | Procede de caracterisation d'une unite de mesure inertielle | |
| EP4437349B1 (fr) | Procédé de limitation de correction de vitesse baro-inertielle et système associé | |
| EP0292339B1 (fr) | Centrale d'attitude integrée pour aérodyne | |
| EP3896398A1 (fr) | Procédé d'identification d'une phase statique d'un véhicule | |
| FR2926637A1 (fr) | Procede et dispositif pour l'estimation de la vitesse par rapport a l'air d'un vehicule aerien | |
| EP1157284A1 (fr) | Dispositif d'hybridation d'un recepteur de positionnement par satellites avec une centrale inertielle | |
| EP3983759B1 (fr) | Procede de surveillance des performances d'unites de mesure inertielle | |
| FR3144274A1 (fr) | Dispositif et procédé de navigation utilisant des données pré-intégrées de façon asynchrone dans une UMI distante | |
| WO2023094761A1 (fr) | Procédé de détection de défaillance d'un baro-altimètre dans une boucle baro-inertielle et système associé | |
| FR3073655B1 (fr) | Procede de determination d'un vecteur vitesse visuel d'un engin mobile, produit programme d'ordinateur et systeme de determination associes | |
| WO2025133244A1 (fr) | Procédé d'estimation de la distance à un objet, calculateur, système et porteur associés | |
| EP4430362A1 (fr) | Procede de navigation hybride inertielle/stellaire a indicateur de performance d'harmonisation |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| EEER | Examination request | ||
| FZDE | Discontinued |