ES2043056T3 - Procedimiento de observacion por barrido de un cuerpo celeste y de medida de una velocidad angular de un vehiculo espacial, sistema de observacion para su puesta en practica, y vehiculo espacial que lo contiene. - Google Patents
Procedimiento de observacion por barrido de un cuerpo celeste y de medida de una velocidad angular de un vehiculo espacial, sistema de observacion para su puesta en practica, y vehiculo espacial que lo contiene.Info
- Publication number
- ES2043056T3 ES2043056T3 ES89401210T ES89401210T ES2043056T3 ES 2043056 T3 ES2043056 T3 ES 2043056T3 ES 89401210 T ES89401210 T ES 89401210T ES 89401210 T ES89401210 T ES 89401210T ES 2043056 T3 ES2043056 T3 ES 2043056T3
- Authority
- ES
- Spain
- Prior art keywords
- space vehicle
- observation
- sweeping
- angular speed
- celestial body
- 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.)
- Expired - Lifetime
Links
- 238000010408 sweeping Methods 0.000 title abstract 3
- 238000000034 method Methods 0.000 title abstract 2
- 230000007704 transition Effects 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
- G01S3/00—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received
- G01S3/78—Direction-finders for determining the direction from which infrasonic, sonic, ultrasonic, or electromagnetic waves, or particle emission, not having a directional significance, are being received using electromagnetic waves other than radio waves
- G01S3/782—Systems for determining direction or deviation from predetermined direction
- G01S3/785—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system
- G01S3/786—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system the desired condition being maintained automatically
- G01S3/7868—Systems for determining direction or deviation from predetermined direction using adjustment of orientation of directivity characteristics of a detector or detector system to give a desired condition of signal derived from that detector or detector system the desired condition being maintained automatically using horizon sensors
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
- B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
- G01P3/64—Devices characterised by the determination of the time taken to traverse a fixed distance
- G01P3/68—Devices characterised by the determination of the time taken to traverse a fixed distance using optical means, i.e. using infrared, visible, or ultraviolet light
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Radar, Positioning & Navigation (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Life Sciences & Earth Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- Electromagnetism (AREA)
- Geochemistry & Mineralogy (AREA)
- Geology (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Navigation (AREA)
- Gyroscopes (AREA)
Abstract
PROCEDIMIENTO DE OBSERVACION POR BARRIDO DE UN CUERPO CELESTE (T) A PARTIR DE UN VEHICULO ESPACIAL (5) COMPORTANDO UN SISTEMA DE OBSERVACION POR BARRIDO POR REFERENCIA A UN EJE DE BARRIDO CARACTERIZADO EN QUE SE FORMAN (16) SUCESIVAMENTE DOS SEÑALES (A, B) CORRESPONDIENDO AL BARRIDO, EN UN MISMO SENTIDO DE DESLIZAMIENTO DE UNA MISMA TOMA DE TIERRA (BT), SE DETECTA (17) EN CADA UNA DE ESTAS SEÑALES UNA TRANSICION CARACTERISTICA (A1, B1) REPRESENTATIVA DE UN MISMO PUNTO CARACTERISTICO DE ESTA TOMA DE TIERRA, SE RECOGE (18) LA POSICION RELATIVA DE ESTAS TRANSICIONES EN ESTAS SEÑALES, Y SE DETERMINA (19) A PARTIR DE UN EVENTUAL DISTANCIAMIENTO ENTRE ESTAS POSICIONES RELATIVAS UNA EVENTUAL VELOCIDAD ANGULAR (W) DEL VEHICULO ESPACIAL, TNEIENDO EN CUENTA EL DISTANCIAMIENTO DE TIEMPO SEPARANDO LOS MOMENTOS DONDE CADA UNA DE ESTAS TRANSICIONES HA APARECIDO EN DICHAS SEÑALES.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8805708A FR2630705B1 (fr) | 1988-04-28 | 1988-04-28 | Procede d'observation par balayage d'un corps celeste et de mesure d'une vitesse angulaire d'un vehicule spatial, systeme d'observation pour sa mise en oeuvre, et vehicule spatial le comportant |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2043056T3 true ES2043056T3 (es) | 1993-12-16 |
Family
ID=9365796
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES89401210T Expired - Lifetime ES2043056T3 (es) | 1988-04-28 | 1989-04-27 | Procedimiento de observacion por barrido de un cuerpo celeste y de medida de una velocidad angular de un vehiculo espacial, sistema de observacion para su puesta en practica, y vehiculo espacial que lo contiene. |
Country Status (7)
Country | Link |
---|---|
US (1) | US5062051A (es) |
EP (1) | EP0341142B1 (es) |
JP (1) | JP2740920B2 (es) |
CA (1) | CA1326529C (es) |
DE (1) | DE68907440T2 (es) |
ES (1) | ES2043056T3 (es) |
FR (1) | FR2630705B1 (es) |
Families Citing this family (13)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2653918B1 (fr) * | 1989-10-31 | 1992-02-14 | Europ Agence Spatiale | Procede de rectification en temps reel des images des satellites meteorologiques geostationnaires. |
US5257760A (en) * | 1992-06-24 | 1993-11-02 | Edo Corporation, Barnes Engineering Division | Scanning earth sensor using the sun's position for determining yaw |
US5546309A (en) * | 1993-10-20 | 1996-08-13 | The Charles Stark Draper Laboratory, Inc. | Apparatus and method for autonomous satellite attitude sensing |
US6732977B1 (en) | 2002-02-11 | 2004-05-11 | Lockheed Martin Corporation | System for on-orbit correction of spacecraft payload pointing errors |
US6695263B1 (en) * | 2002-02-12 | 2004-02-24 | Lockheed Martin Corporation | System for geosynchronous spacecraft rapid earth reacquisition |
US7051980B2 (en) * | 2002-02-26 | 2006-05-30 | Lockheed Martin Corporation | Efficient orbit sparing system for space vehicle constellations |
US6702234B1 (en) | 2002-03-29 | 2004-03-09 | Lockheed Martin Corporation | Fault tolerant attitude control system for zero momentum spacecraft |
US7835826B1 (en) | 2005-12-13 | 2010-11-16 | Lockheed Martin Corporation | Attitude determination system for yaw-steering spacecraft |
JP4820976B2 (ja) * | 2006-10-06 | 2011-11-24 | 株式会社指月電機製作所 | トランスコアの固定構造 |
US8767072B1 (en) * | 2010-03-26 | 2014-07-01 | Lockheed Martin Corporation | Geoposition determination by starlight refraction measurement |
CN106225807A (zh) * | 2016-07-27 | 2016-12-14 | 中国科学院长春光学精密机械与物理研究所 | 视频卫星对地面区域目标进行凝视成像的仿真方法及系统 |
US10612901B2 (en) * | 2018-03-23 | 2020-04-07 | Simmonds Precision Products, Inc. | Real-time compensation of inertial gyroscopes |
CN111897357B (zh) * | 2020-08-13 | 2023-10-20 | 上海航天控制技术研究所 | 一种卫星对地扫描的姿态跟踪控制方法 |
Family Cites Families (24)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CA633497A (en) * | 1961-12-26 | Collins Radio Company | Satellite apparent position computer | |
US2998529A (en) * | 1958-06-19 | 1961-08-29 | Kollsman Instr Corp | Automatic astrocompass |
US3012728A (en) * | 1958-07-23 | 1961-12-12 | Collins Radio Co | Satellite apparent position computer |
US3216674A (en) * | 1959-06-08 | 1965-11-09 | Walter G Finch | Proportional navigation system for a spinning body in free space |
US3310982A (en) * | 1961-08-31 | 1967-03-28 | United Aircraft Corp | Navigation system with vehicle motion signals modified by drift angle signals |
US3576999A (en) * | 1965-01-16 | 1971-05-04 | Bendix Corp | Method and apparatus for determining the orientation of an object relative to an elliptic object |
US3535521A (en) * | 1966-02-28 | 1970-10-20 | Itt | Satellite attitude control utilizing a plurality of infrared sensors |
US3769710A (en) * | 1969-04-01 | 1973-11-06 | R Reister | Electronic celestial navigation means |
FR2246843B1 (es) * | 1973-10-04 | 1976-05-14 | Sodern | |
US4328421A (en) * | 1980-02-25 | 1982-05-04 | Barnes Engineering Company | Horizon sensor |
US4617634A (en) * | 1983-06-28 | 1986-10-14 | Mitsubishi Denki Kabushiki Kaisha | Artificial satellite attitude control system |
JPS6025900A (ja) * | 1983-07-25 | 1985-02-08 | 株式会社日立製作所 | スタ−センサによる姿勢決定システム |
DE3330861A1 (de) * | 1983-08-26 | 1985-03-14 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Vorrichtung zur feststellung von lageaenderungen eines raumflugkoerpers |
JPS60104499A (ja) * | 1983-11-11 | 1985-06-08 | 株式会社日立製作所 | 姿勢決定方式 |
DE3422007C2 (de) * | 1984-06-14 | 1986-10-02 | Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn | Anordnung für einen Erdhorizontsensor eines in einem Orbit befindlichen Erdsatelliten |
US4837699A (en) * | 1985-07-18 | 1989-06-06 | Hughes Aircraft Company | Method for controlling the spin axis attitude of a spinning spacecraft |
US4801202A (en) * | 1985-12-20 | 1989-01-31 | Itt Aerospace Optical | Method and apparatus for radiometer star sensing |
SE461835B (sv) * | 1986-02-13 | 1990-04-02 | Sparring Elfa Ab | Hjulfaeste foer monterbara moebeldelar |
US4688092A (en) * | 1986-05-06 | 1987-08-18 | Ford Aerospace & Communications Corporation | Satellite camera image navigation |
US4827422A (en) * | 1986-12-04 | 1989-05-02 | Barnes Engineering Company | Fan scan horizon sensor for a spin stabilized satellite |
US4912475A (en) * | 1987-03-20 | 1990-03-27 | Massachusetts Institute Of Technology | Techniques for determining orbital data |
FR2615477B1 (fr) * | 1987-05-22 | 1989-08-18 | Centre Nat Etd Spatiales | Dispositif et procede de pointage d'une sonde spatiale vers un corps celeste |
US4944587A (en) * | 1988-03-17 | 1990-07-31 | Kabushiki Kaisha Toshiba | Star sensor |
GB8809247D0 (en) * | 1988-04-20 | 1988-05-25 | British Aerospace | Attitude recovery for spacecraft |
-
1988
- 1988-04-28 FR FR8805708A patent/FR2630705B1/fr not_active Expired - Fee Related
-
1989
- 1989-04-25 CA CA000597737A patent/CA1326529C/en not_active Expired - Fee Related
- 1989-04-27 ES ES89401210T patent/ES2043056T3/es not_active Expired - Lifetime
- 1989-04-27 DE DE89401210T patent/DE68907440T2/de not_active Expired - Fee Related
- 1989-04-27 EP EP89401210A patent/EP0341142B1/fr not_active Expired - Lifetime
- 1989-04-28 JP JP1111895A patent/JP2740920B2/ja not_active Expired - Lifetime
- 1989-05-01 US US07/345,592 patent/US5062051A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2630705A1 (fr) | 1989-11-03 |
FR2630705B1 (fr) | 1990-08-24 |
DE68907440T2 (de) | 1993-11-04 |
JPH0249111A (ja) | 1990-02-19 |
US5062051A (en) | 1991-10-29 |
JP2740920B2 (ja) | 1998-04-15 |
CA1326529C (en) | 1994-01-25 |
EP0341142A2 (fr) | 1989-11-08 |
EP0341142A3 (en) | 1989-11-15 |
EP0341142B1 (fr) | 1993-07-07 |
DE68907440D1 (de) | 1993-08-12 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
ES2043056T3 (es) | Procedimiento de observacion por barrido de un cuerpo celeste y de medida de una velocidad angular de un vehiculo espacial, sistema de observacion para su puesta en practica, y vehiculo espacial que lo contiene. | |
Wardle et al. | The Radio Structure of Quasars. II. | |
RU95108883A (ru) | Вспомогательное посадочное устройство | |
SE8504299D0 (sv) | Sett for navigering av en forarlos farkost | |
FR2623626B1 (fr) | Dispositif de controle non destructif de tubes par ultrasons | |
NO148727C (no) | Fremgangsmaate for bestemmelse av det organisk bundne svovel i en liten proeve av geologiske sedimenter | |
NO901349D0 (no) | Fremgangsmaate for maaling eller testing. | |
ATE110549T1 (de) | Analyse von oberflächenschwingungen. | |
FR2610110B1 (fr) | Dispositif de detection de defauts structurels | |
AT355086B (de) | Vorrichtung zur ueberbrueckung der dehnungsfugen in fahrbahnen u. dgl. insbesondere in brueckenfahrbahnen | |
DE68912151D1 (de) | Elektrochemische Sensoren für immunologische Testverfahren. | |
DK0382592T3 (da) | Universielt kartografisk afbildningssystem, især til visualisering på et passende baggrundskort af et objekt, der er indmålt på vilkårlig måde | |
FI890266A (fi) | Foerfarande foer framstaellning av affino-enzymatiska foereningar, vilka anvaends foer visuell bestaemning av kolesterol pao hudytan. | |
SU705344A1 (ru) | Устройство дл измерени направлени воздушного потока | |
DE3586703D1 (de) | Aufklaerungssystem. | |
SU1763891A1 (ru) | Способ измерени углов между направлени ми на отражатели | |
RU2099749C1 (ru) | Устройство для обнаружения в природе светоносного эфира и определения скорости перемещения в нем материальных объектов | |
Hoffmann | The visibility range when observing an aircraft with and without field-glasses | |
SU434364A1 (ru) | Устройство для имитации движения земной поверхности | |
Dollfus | New optical measurements of planetary diameters V. Planet Mercury | |
US1179242A (en) | Protractor. | |
SU746166A1 (ru) | Способ получени абразивной поверхности дл испытани материалов на износ | |
NO893448L (no) | Hastighetsmaaler med retningsindikator for vegtunneler. | |
FR2365782A1 (fr) | Dispositif pour la mesure, a distance, d'un ecart angulaire au moyen de sources electro-optiques de forme geometrique definie | |
SU1421974A1 (ru) | Способ измерени размеров детали |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
Ref document number: 341142 Country of ref document: ES |