FR2448713A1 - GYROSCOPIC COMPASS - Google Patents
GYROSCOPIC COMPASSInfo
- Publication number
- FR2448713A1 FR2448713A1 FR8002695A FR8002695A FR2448713A1 FR 2448713 A1 FR2448713 A1 FR 2448713A1 FR 8002695 A FR8002695 A FR 8002695A FR 8002695 A FR8002695 A FR 8002695A FR 2448713 A1 FR2448713 A1 FR 2448713A1
- Authority
- FR
- France
- Prior art keywords
- axis
- gyroscope
- plane
- place
- cancel
- 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.)
- Granted
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/02—Rotary gyroscopes
- G01C19/34—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes
- G01C19/38—Rotary gyroscopes for indicating a direction in the horizontal plane, e.g. directional gyroscopes with north-seeking action by other than magnetic means, e.g. gyrocompasses using earth's rotation
Landscapes
- Life Sciences & Earth Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geology (AREA)
- Physics & Mathematics (AREA)
- Engineering & Computer Science (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- Gyroscopes (AREA)
Abstract
COMPAS GYROSCOPIQUE A DEUX AXES SENSIBLES ORTHOGONAUX X ET Y POUR DETERMINER LA DIRECTION D'UN POINT CARDINAL, PARTICULIEREMENT DU NORD. L'APPAREIL ETANT SITUE EN UN LIEU DE LATITUDEA, ET LA VERTICALE DU LIEU FAISANT UN ANGLEB AVEC L'AXE DE ROTATION Z DU GYROSCOPE, L'AXE Y EST AMENE ET MAINTENU AVEC PRECISION DANS LE PLAN HORIZONTAL DU LIEU ET POINTE NOMINALEMENT DANS LA DIRECTION EST-OUEST, L'ANGLE D'ECART D'ALIGNEMENT, DESIGNE PARG, ETANT DEJA FAIBLE. ON VEUT ANNULER CET ECART EN FAISANT VIRER LE GYROSCOPE AUTOUR DE SON AXE Z, ET AMENER AINSI LE PLAN AZIMUTAL DE L'AXE X A SE CONFONDRE AVEC LE PLAN MERIDIEN. LES AXESX ET Y SONT EQUIPES DE CAPTEURS DE POSITION ANGULAIRE XP ET YP DONT LES SIGNAUX SORTANTS AMPLIFIES XO ET YO SONT APPLIQUES D'UNE PART A DES GENERATEURS DE COUPLE XT ET YT AGISSANT RESPECTIVEMENT SUR LES CAGES EXTERNE ET INTERNE DU GYROSCOPE, ET D'AUTRE PART, A TRAVERS DES UNITES DE TRAITEMENT 30 ET 31, A UN AMPLIFICATEUR DE SOMMATION ETOU D'INTEGRATION 32 SUIVI D'UN INDICATEUR 33 AFFICHANT L'ANGLEG. L'OPERATEUR FAIT VIRER LE GYROSCOPE JUSQU'A L'ANNULATION DE L'ANGLE AFFICHE, AMENANT AINSI L'AXE X DANS LE PLAN MERIDIEN DU LIEU. APPLICATION A LA DETERMINATION DU NORD GEOGRAPHIQUE.GYROSCOPIC COMPASS WITH TWO SENSITIVE ORTHOGONAL X AND Y AXES TO DETERMINE THE DIRECTION OF A CARDINAL POINT, ESPECIALLY FROM THE NORTH. THE EQUIPMENT BEING LOCATED IN A PLACE OF LATITUDEA, AND THE VERTICAL OF THE PLACE MAKING AN ANGLEB WITH THE Z-AXIS OF THE GYROSCOPE, THE AXIS IS BROUGHT THERE AND MAINTAINED WITH PRECISION IN THE HORIZONTAL PLANE OF THE PLACE AND POINTS NOMINALLY IN THE DIRECTION EAST-WEST, THE RIGHT-OF-RUN ANGLE, DESIGNATED PARG, IS ALREADY LOW. WE WANT TO CANCEL THIS DIFFERENCE BY TURNING THE GYROSCOPE AROUND ITS Z-AXIS, AND THUS BRINGING THE AZIMUTAL PLANE OF THE X-AXIS TO MIX WITH THE MERIDIEN PLANE. THE AXESX AND Y ARE EQUIPPED WITH ANGULAR POSITION SENSORS XP AND YP WHOSE AMPLIFIED OUTPUT SIGNALS XO AND YO ARE APPLIED ON THE ONE HAND TO XT AND YT TORQUE GENERATORS ACTING RESPECTIVELY ON THE EXTERNAL AND INTERNAL CAGES OF THE GYROSCOPE, AND OF ' ON THE OTHER HAND, THROUGH PROCESSING UNITS 30 AND 31, TO A SUMMATION AND OR INTEGRATION AMPLIFIER 32 MONITORING AN INDICATOR 33 DISPLAYING ANGLEG. THE OPERATOR TURNS THE GYROSCOPE UNTIL THE DISPLAYED ANGLE IS CANCEL, THUS BRINGING THE X-AXIS INTO THE MERIDIAN PLANE OF THE SITE. APPLICATION TO THE DETERMINATION OF THE GEOGRAPHICAL NORTH.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7904700A GB2041519B (en) | 1979-02-09 | 1979-02-09 | Gyroscopic apparatus |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2448713A1 true FR2448713A1 (en) | 1980-09-05 |
FR2448713B1 FR2448713B1 (en) | 1984-01-06 |
Family
ID=10503102
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8002695A Granted FR2448713A1 (en) | 1979-02-09 | 1980-02-07 | GYROSCOPIC COMPASS |
Country Status (4)
Country | Link |
---|---|
JP (1) | JPS55106309A (en) |
DE (1) | DE3004007A1 (en) |
FR (1) | FR2448713A1 (en) |
GB (1) | GB2041519B (en) |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH407564A (en) * | 1962-10-30 | 1966-02-15 | Filotecnica Salmoiraghi Spa | Gyroteodolite for azimuthal measurements referring to geographic north |
US3279086A (en) * | 1963-08-29 | 1966-10-18 | Bell Aerospace Corp | Compensated gyroscopic directional reference |
-
1979
- 1979-02-09 GB GB7904700A patent/GB2041519B/en not_active Expired
-
1980
- 1980-02-04 DE DE19803004007 patent/DE3004007A1/en active Granted
- 1980-02-07 FR FR8002695A patent/FR2448713A1/en active Granted
- 1980-02-08 JP JP1376080A patent/JPS55106309A/en active Granted
Also Published As
Publication number | Publication date |
---|---|
DE3004007A1 (en) | 1980-09-11 |
FR2448713B1 (en) | 1984-01-06 |
JPS6216363B2 (en) | 1987-04-13 |
JPS55106309A (en) | 1980-08-15 |
GB2041519A (en) | 1980-09-10 |
GB2041519B (en) | 1983-05-11 |
DE3004007C2 (en) | 1988-07-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |