INTEGRATED INERTIAL STELLAR ATTITUDE SENSOR
An integrated inertial stellar attitude sensor for an aerospace vehicle includes a star camera system (12), a gyroscope system (14), a controller system (16) for synchronously integrating an output of said star camera system (12) and an output of said gyroscope system (14) into a stream of data (C),...
Saved in:
| Main Authors | , , |
|---|---|
| Format | Patent |
| Language | English French |
| Published |
02.09.2004
|
| Edition | 7 |
| Subjects | |
| Online Access | Get full text |
Cover
Loading…
| Abstract | An integrated inertial stellar attitude sensor for an aerospace vehicle includes a star camera system (12), a gyroscope system (14), a controller system (16) for synchronously integrating an output of said star camera system (12) and an output of said gyroscope system (14) into a stream of data (C), and a flight computer (18) responsive to said stream of data for determining from the star camera system output and the gyroscope system output attitude of the aerospace vehicle.
Capteur inertiel intégré d'attitude stellaire pour véhicule aérospatial. Il comprend un système de caméra pour étoiles, un système de gyroscope, un système de contrôleur destiné à intégrer de façon synchrone une sortie de ladite caméra pour étoiles, un système de gyroscope, un système de contrôleur pour intégrer de façon synchrone une sortie de ladite caméra pour étoiles et une sortie dudit gyroscope en un flux de données, et un ordinateur de bord réagissant audit flux de données pour déterminer à partir de la sortie du système de caméra pour étoiles et de sortie de la système de gyroscope l'attitude du véhicule aérospatial. |
|---|---|
| AbstractList | An integrated inertial stellar attitude sensor for an aerospace vehicle includes a star camera system (12), a gyroscope system (14), a controller system (16) for synchronously integrating an output of said star camera system (12) and an output of said gyroscope system (14) into a stream of data (C), and a flight computer (18) responsive to said stream of data for determining from the star camera system output and the gyroscope system output attitude of the aerospace vehicle.
Capteur inertiel intégré d'attitude stellaire pour véhicule aérospatial. Il comprend un système de caméra pour étoiles, un système de gyroscope, un système de contrôleur destiné à intégrer de façon synchrone une sortie de ladite caméra pour étoiles, un système de gyroscope, un système de contrôleur pour intégrer de façon synchrone une sortie de ladite caméra pour étoiles et une sortie dudit gyroscope en un flux de données, et un ordinateur de bord réagissant audit flux de données pour déterminer à partir de la sortie du système de caméra pour étoiles et de sortie de la système de gyroscope l'attitude du véhicule aérospatial. |
| Author | BRADY, TYE, M KOUREPENIS, ANTHONY, S WYMAN, WILLIAM, F., JR |
| Author_xml | – fullname: BRADY, TYE, M – fullname: KOUREPENIS, ANTHONY, S – fullname: WYMAN, WILLIAM, F., JR |
| BookMark | eNrjYmDJy89L5WTQ9vQLcXUPcgxxdVHw9HMNCvF09FEIDnH18XEMUnAMCfEMCXVxVQh29Qv2D-JhYE1LzClO5YXS3AzKbq4hzh66qQX58anFBYnJqXmpJfHh_kYGBiYGBuZGFuaOxsbEqQIAGLwn1A |
| ContentType | Patent |
| DBID | EVB |
| DatabaseName | esp@cenet |
| DatabaseTitleList | |
| Database_xml | – sequence: 1 dbid: EVB name: esp@cenet url: http://worldwide.espacenet.com/singleLineSearch?locale=en_EP sourceTypes: Open Access Repository |
| DeliveryMethod | fulltext_linktorsrc |
| Discipline | Medicine Chemistry Sciences Physics |
| DocumentTitleAlternate | CAPTEUR INERTIEL INTEGRE D'ATTITUDE STELLAIRE |
| Edition | 7 |
| ExternalDocumentID | WO2004007287A3 |
| GroupedDBID | EVB |
| ID | FETCH-epo_espacenet_WO2004007287A33 |
| IEDL.DBID | EVB |
| IngestDate | Fri Jul 19 14:27:41 EDT 2024 |
| IsOpenAccess | true |
| IsPeerReviewed | false |
| IsScholarly | false |
| Language | English French |
| LinkModel | DirectLink |
| MergedId | FETCHMERGED-epo_espacenet_WO2004007287A33 |
| Notes | Application Number: WO2003US22150 |
| OpenAccessLink | https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20040902&DB=EPODOC&CC=WO&NR=2004007287A3 |
| ParticipantIDs | epo_espacenet_WO2004007287A3 |
| PublicationCentury | 2000 |
| PublicationDate | 20040902 |
| PublicationDateYYYYMMDD | 2004-09-02 |
| PublicationDate_xml | – month: 09 year: 2004 text: 20040902 day: 02 |
| PublicationDecade | 2000 |
| PublicationYear | 2004 |
| RelatedCompanies | THE CHARLES STARK DRAPER LABORATORY, INC |
| RelatedCompanies_xml | – name: THE CHARLES STARK DRAPER LABORATORY, INC |
| Score | 2.6067445 |
| Snippet | An integrated inertial stellar attitude sensor for an aerospace vehicle includes a star camera system (12), a gyroscope system (14), a controller system (16)... |
| SourceID | epo |
| SourceType | Open Access Repository |
| SubjectTerms | AIRCRAFT AVIATION COSMONAUTICS GYROSCOPIC INSTRUMENTS MEASURING MEASURING DISTANCES, LEVELS OR BEARINGS NAVIGATION PERFORMING OPERATIONS PHOTOGRAMMETRY OR VIDEOGRAMMETRY PHYSICS SURVEYING TESTING TRANSPORTING VEHICLES OR EQUIPMENT THEREFOR |
| Title | INTEGRATED INERTIAL STELLAR ATTITUDE SENSOR |
| URI | https://worldwide.espacenet.com/publicationDetails/biblio?FT=D&date=20040902&DB=EPODOC&locale=&CC=WO&NR=2004007287A3 |
| hasFullText | 1 |
| inHoldings | 1 |
| isFullTextHit | |
| isPrint | |
| link | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV1LS8NAEB5qfd40Kj6qBJRcJJjHptFDkTTZ2EialDRqb6XZbECQtNiIf9_ZtNWeet2B2Qd889j9Zhbg1iBFYXGLqUbbYCphBCFVaJaaZZmdm_rk0dZEvXM_avdeycvIGjXgc1ULU_cJ_ambIyKiGOK9qu317P8Sy6u5lfP77AOHpk9-2vGUVXZMBM1Q8bodOoi92FVcF_M2JUoWMs3G_MAxt2BbBNKi0z5964q6lNm6U_EPYWeA-srqCBq8lGDfXf29JsFef_nkLcFuzdFkcxxc4nB-DHeik-1z4qDZkYOIJmnghPIwpWHoJLKTpgHGeVQe0mgYJydw49PU7ak4__hvu-P3eH2x5ik0y2nJz0DOia1xk-VE5zrBNCGzOHswMODXcm5phJxDa5Omi83iSzhYsFIEf6oFzerrm1-hw62y6_qcfgGUyX6R |
| link.rule.ids | 230,309,786,891,25594,76904 |
| linkProvider | European Patent Office |
| linkToHtml | http://utb.summon.serialssolutions.com/2.0.0/link/0/eLvHCXMwfV1LT8JAEJ4gPvCmqPGB2kTTi2lc2i2VAzGlXaRaWlJW5EbsdklMTCFS4993WkA5cd1JZh_JNzPf7swswK1OJxNTmkLTG7rQqKAIqQkxtTiOrcSovzctktc794JG95U-j8xRCT5XtTBFn9CfojkiIkog3rPCXs_-L7HcIrdyfh9_4ND0scNbrrpixzRPM1Tddov1Qzd0VMdB3qYG0UJGLOQHtrEF2xaSwrzTPhu287qU2bpT6RzATh_1pdkhlGRahYqz-nutCnu95ZN3FXaLHE0xx8ElDudHcJd3sn2KbDQ7ihewiHu2rww48307UmzOPYzzmDJgwSCMjuGmw7jT1XD-8d92x2_h-mKNEyin01SegpJQi0hDJLQu6xRpQmxK8aBjwE8SaRJKz6C2SdP5ZvE1VLq85499L3i5gP1FhkpTI3oNytnXt7xE55vFV8WZ_QKmGoF9 |
| openUrl | ctx_ver=Z39.88-2004&ctx_enc=info%3Aofi%2Fenc%3AUTF-8&rfr_id=info%3Asid%2Fsummon.serialssolutions.com&rft_val_fmt=info%3Aofi%2Ffmt%3Akev%3Amtx%3Apatent&rft.title=INTEGRATED+INERTIAL+STELLAR+ATTITUDE+SENSOR&rft.inventor=BRADY%2C+TYE%2C+M&rft.inventor=KOUREPENIS%2C+ANTHONY%2C+S&rft.inventor=WYMAN%2C+WILLIAM%2C+F.%2C+JR&rft.date=2004-09-02&rft.externalDBID=A3&rft.externalDocID=WO2004007287A3 |