DE3671875D1 - In zwei alternativen flugweisen operierendes raumfahrzeug. - Google Patents
In zwei alternativen flugweisen operierendes raumfahrzeug.Info
- Publication number
- DE3671875D1 DE3671875D1 DE8686301554T DE3671875T DE3671875D1 DE 3671875 D1 DE3671875 D1 DE 3671875D1 DE 8686301554 T DE8686301554 T DE 8686301554T DE 3671875 T DE3671875 T DE 3671875T DE 3671875 D1 DE3671875 D1 DE 3671875D1
- Authority
- DE
- Germany
- Prior art keywords
- spacecraft
- oriented
- control means
- vehicle operating
- space vehicle
- 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 - Fee Related
Links
- 230000005484 gravity Effects 0.000 abstract 2
- 230000006641 stabilisation Effects 0.000 abstract 2
- 238000011105 stabilization Methods 0.000 abstract 2
Classifications
-
- 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
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
-
- 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
- B64G1/244—Spacecraft control systems
-
- 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
- B64G1/34—Guiding or controlling apparatus, e.g. for attitude control using gravity gradient
-
- 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
-
- 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
- B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun 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
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S136/00—Batteries: thermoelectric and photoelectric
- Y10S136/291—Applications
- Y10S136/292—Space - satellite
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Aviation & Aerospace Engineering (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Chemical & Material Sciences (AREA)
- Automation & Control Theory (AREA)
- Life Sciences & Earth Sciences (AREA)
- Environmental & Geological Engineering (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Geology (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Radio Relay Systems (AREA)
- Vehicle Waterproofing, Decoration, And Sanitation Devices (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US06/713,816 US4728061A (en) | 1985-03-20 | 1985-03-20 | Spacecraft operable in two alternative flight modes |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3671875D1 true DE3671875D1 (de) | 1990-07-19 |
Family
ID=24867657
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8686301554T Expired - Fee Related DE3671875D1 (de) | 1985-03-20 | 1986-03-05 | In zwei alternativen flugweisen operierendes raumfahrzeug. |
Country Status (6)
Country | Link |
---|---|
US (1) | US4728061A (de) |
EP (1) | EP0195553B1 (de) |
JP (1) | JPS61268600A (de) |
AT (1) | ATE53551T1 (de) |
CA (1) | CA1326655C (de) |
DE (1) | DE3671875D1 (de) |
Families Citing this family (39)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JPH0725358B2 (ja) * | 1987-09-08 | 1995-03-22 | 三菱電機株式会社 | 宇宙飛しょう体の姿勢制御装置 |
JPH0725359B2 (ja) * | 1987-10-08 | 1995-03-22 | 三菱電機株式会社 | 宇宙飛しよう体の姿勢制御装置 |
US4960250A (en) * | 1988-09-12 | 1990-10-02 | Space Industries Partnership, L.P. | Energy desaturation of electromechanical actuators used in satellite attitude control |
FR2637565B1 (fr) * | 1988-10-06 | 1991-01-11 | Aerospatiale | Systeme de controle actif selon trois axes de l'attitude d'un satellite geostationnaire |
US5183225A (en) * | 1989-01-09 | 1993-02-02 | Forward Robert L | Statite: spacecraft that utilizes sight pressure and method of use |
US5092543A (en) * | 1989-09-27 | 1992-03-03 | General Electric Company | Spacecraft attitude control with avoidance constraint |
US5271582A (en) * | 1990-06-29 | 1993-12-21 | Standard Space Platforms Corp. | Modular mother satellite bus for subsidiary payloads |
US5152482A (en) * | 1990-06-29 | 1992-10-06 | Standard Space Platforms Corp. | Modular mother satellite bus for subsidiary payloads |
FR2669887B1 (fr) * | 1990-11-30 | 1995-06-02 | Aerospatiale | Procede de controle d'attitude en tangage d'un satellite grace a la pression de radiation solaire et satellite adapte a sa mise en óoeuvre. |
US5762298A (en) * | 1991-03-27 | 1998-06-09 | Chen; Franklin Y. K. | Use of artificial satellites in earth orbits adaptively to modify the effect that solar radiation would otherwise have on earth's weather |
DE4114804A1 (de) * | 1991-05-07 | 1992-11-12 | Messerschmitt Boelkow Blohm | Vorrichtung zur lageregelung von satelliten mit solardruckmomenten |
US5228644A (en) * | 1991-05-28 | 1993-07-20 | The United States Of America As Represented By The United States National Aeronautics And Space Administration | Solar powered system for a space vehicle |
JPH0577797A (ja) * | 1991-09-19 | 1993-03-30 | Nec Corp | 人工衛星装置 |
US5377936A (en) * | 1992-03-19 | 1995-01-03 | Mitchell; Maurice | Net kinetic energy differential guidance and propulsion system for satellites and space vehicles |
US5310144A (en) * | 1992-07-06 | 1994-05-10 | Hughes Aircraft Company | Method and apparatus for satellite torque balancing |
WO1994006680A1 (en) * | 1992-09-23 | 1994-03-31 | Space Industries, Inc. | Spacecraft berthing mechanism |
FR2710314B1 (fr) * | 1993-09-23 | 1995-12-15 | Aerospatiale | Satellite stabilisé 3-axes à pointage géocentrique en orbite basse à générateur solaire orientable 1-axe. |
US5546309A (en) * | 1993-10-20 | 1996-08-13 | The Charles Stark Draper Laboratory, Inc. | Apparatus and method for autonomous satellite attitude sensing |
DE69428773T2 (de) * | 1994-02-04 | 2002-07-11 | Orbital Sciences Corp., Dulles | Sich selbst entfaltende Wendelstruktur |
US5669586A (en) * | 1994-12-06 | 1997-09-23 | Space Systems/Loral, Inc. | Satellite gravity gradient compensation using on-orbit solar array reorientation |
FR2748721A1 (fr) * | 1996-05-17 | 1997-11-21 | Matra Marconi Space France | Appareil de reglage de la rotation d'un vaisseau spatial autour d'un axe |
US5895014A (en) * | 1996-07-31 | 1999-04-20 | Hughes Electronics Corporation | Satellite solar array and method of biasing to reduce seasonal output power fluctuations |
US6068218A (en) * | 1997-05-14 | 2000-05-30 | Hughes Electronics Corporation | Agile, spinning spacecraft with sun-steerable solar cell array and method |
US6227497B1 (en) * | 1998-08-19 | 2001-05-08 | Mobile Communications Holdings, Inc. | Adaptively positioned solar array |
US6474602B1 (en) * | 2000-04-27 | 2002-11-05 | Hughes Electronics Corporation | Spacecraft pointing performance via optimized solar array orientation |
US6585193B1 (en) | 2000-10-30 | 2003-07-01 | Lockheed Martin Corporation | Spacecraft with integrated pulsed-plasma thrusters |
US7823836B2 (en) * | 2006-12-04 | 2010-11-02 | The Boeing Company | Optimal sun safe attitude for satellite ground tracking |
US20130008488A1 (en) * | 2011-07-07 | 2013-01-10 | Holmes John W | Use of rotating photovoltaic cells and assemblies for concentrated and non-concentrated solar systems |
RU2565426C2 (ru) * | 2014-03-12 | 2015-10-20 | Акционерное общество "Ракетно-космический центр "Прогресс" (АО "РКЦ "Прогресс") | Способ ориентации космических аппаратов и устройство его реализующее |
US10005568B2 (en) | 2015-11-13 | 2018-06-26 | The Boeing Company | Energy efficient satellite maneuvering |
JP6537462B2 (ja) * | 2016-02-12 | 2019-07-03 | 三菱電機株式会社 | 衛星自律制御装置、人工衛星、衛星管理システム、衛星自律制御方法及び衛星自律制御プログラム |
JP6817341B2 (ja) | 2016-06-14 | 2021-01-20 | ブロムクイスト、リチャード | 宇宙船及び制御方法 |
ES2955054T3 (es) | 2017-09-10 | 2023-11-28 | Orbit Fab Inc | Sistemas y métodos para suministrar, almacenar, y procesar materiales en el espacio |
US11273932B2 (en) | 2017-09-10 | 2022-03-15 | Space Arena, Inc. | Enclosures for facilitating activities in space, and associated systems and methods |
US11034235B2 (en) | 2017-12-06 | 2021-06-15 | Orbit Fab, Inc. | Systems and methods for creating and automating an enclosed volume with a flexible fuel tank and propellant metering for machine operations |
RU2685948C1 (ru) * | 2018-04-02 | 2019-04-23 | ООО "Инжиниринговый центр микроспутниковых компетенций" | Способ пространственной ориентации микроспутника |
US11471717B1 (en) * | 2018-12-31 | 2022-10-18 | Vlad Novotny | Early fire detection and suppression |
JP6750913B1 (ja) * | 2019-12-24 | 2020-09-02 | 一般財団法人グローバルヘルスケア財団 | 宇宙航行体 |
DE102022114410A1 (de) | 2022-06-08 | 2023-12-14 | Mt Aerospace Ag | Zentralrohr für Satelliten und Raumfahrzeuge |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3168263A (en) * | 1961-11-20 | 1965-02-02 | Gen Dynamics Corp | Gravity gradient satellite orientation system |
US3145948A (en) * | 1962-07-09 | 1964-08-25 | Richard B Kershner | Satellite rotation by radiation pressure |
US3243143A (en) * | 1962-11-27 | 1966-03-29 | Gen Electric | Doubly stabilized satellite |
US3241142A (en) * | 1962-12-28 | 1966-03-15 | Litton Systems Inc | Gravity stabilized satellite |
US3148846A (en) * | 1963-01-07 | 1964-09-15 | Robert R Newton | System for gravity orienting a satellite |
FR1375558A (fr) * | 1963-11-27 | 1964-10-16 | Thomson Houston Comp Francaise | Perfectionnements aux procédés de stabilisation des véhicules spatiaux |
US3268183A (en) * | 1963-12-12 | 1966-08-23 | Etkin Bernard | Passive stabilization of an earth's satellite |
US3367604A (en) * | 1964-04-10 | 1968-02-06 | Gen Electric | Extensible straight rod-like structure |
US3282532A (en) * | 1964-07-27 | 1966-11-01 | Bruce E Tinling | Stabilization of gravity oriented satellites |
US3302905A (en) * | 1964-08-06 | 1967-02-07 | Gen Electric | Stabilized satellite |
US3500417A (en) * | 1965-05-25 | 1970-03-10 | Sichak Associates | Steered-cone retrodirective antenna |
US3429525A (en) * | 1965-09-24 | 1969-02-25 | Westinghouse Electric Corp | Satellite orientation apparatus |
US3362656A (en) * | 1965-11-22 | 1968-01-09 | Navy Usa | Damping coupler for satellite attitude control |
US3480232A (en) * | 1965-11-22 | 1969-11-25 | Us Navy | Damping coupler for satellite attitude control |
US3386686A (en) * | 1967-01-19 | 1968-06-04 | Nasa Usa | Station keeping of a gravity-gradient stabilized satellite |
US3519222A (en) * | 1967-01-27 | 1970-07-07 | Goodyear Aerospace Corp | Augmented gravity gradient satellite stabilization system |
US3640487A (en) * | 1967-07-13 | 1972-02-08 | Gen Electric | Vertical orientation device |
US3768756A (en) * | 1967-09-21 | 1973-10-30 | Westinghouse Electric Corp | Commandable satellite attitude control apparatus |
US3601338A (en) * | 1967-11-17 | 1971-08-24 | Tokyo Shibaura Electric Co | Apparatus for controlling the attitude of a satellite |
US3516622A (en) * | 1968-02-05 | 1970-06-23 | Gen Electric | Longitude keeper |
US3567155A (en) * | 1968-12-20 | 1971-03-02 | James A Gatlin | Gravity gradient attitude control system |
US3540676A (en) * | 1968-12-20 | 1970-11-17 | Nasa | Redundant actuating mechanism |
US3635425A (en) * | 1969-10-01 | 1972-01-18 | Us Navy | Deployment method for a telescoping solar array |
US3582020A (en) * | 1969-12-01 | 1971-06-01 | Gen Dynamics Corp | Gravity gradient satellite orientation system for high pointing accuracy |
FR2476018A1 (fr) * | 1980-02-14 | 1981-08-21 | Org Europeene De Rech | Configuration de satellites pour mission geostationnaire |
-
1985
- 1985-03-20 US US06/713,816 patent/US4728061A/en not_active Expired - Lifetime
-
1986
- 1986-03-04 CA CA000503214A patent/CA1326655C/en not_active Expired - Fee Related
- 1986-03-05 EP EP86301554A patent/EP0195553B1/de not_active Expired - Lifetime
- 1986-03-05 AT AT86301554T patent/ATE53551T1/de not_active IP Right Cessation
- 1986-03-05 DE DE8686301554T patent/DE3671875D1/de not_active Expired - Fee Related
- 1986-03-20 JP JP61063856A patent/JPS61268600A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
ATE53551T1 (de) | 1990-06-15 |
EP0195553A3 (en) | 1987-09-16 |
JPH0583440B2 (de) | 1993-11-26 |
EP0195553A2 (de) | 1986-09-24 |
EP0195553B1 (de) | 1990-06-13 |
CA1326655C (en) | 1994-02-01 |
JPS61268600A (ja) | 1986-11-28 |
US4728061A (en) | 1988-03-01 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
DE3671875D1 (de) | In zwei alternativen flugweisen operierendes raumfahrzeug. | |
GB1554203A (en) | Momentum biased active three-axis satellite attitude control system | |
FR2710314B1 (fr) | Satellite stabilisé 3-axes à pointage géocentrique en orbite basse à générateur solaire orientable 1-axe. | |
EP0189051A3 (en) | Storing arrangement for vehicles, particularly in the area of the transmission tunnel for lorries | |
DE3671730D1 (de) | Aerodynamische verkleidung an der unterseite von personenwagen. | |
DE3669399D1 (de) | Anordnung in luftfahrzeugen zur erzeugung dreifacher redundanz fuer wenigstens zwei achsen im raum bei der fluglageregelung und -stabilisierung. | |
CARL | System Design and Integration Panel Workshop summary(large space structures and associated propulsion systems) | |
SU943933A1 (ru) | Устройство стабилизации объекта,установленного на транспортном средстве | |
FRENCH | An overview of Mars surface mobility justification and options | |
Maskell | An extended Kalman filter integrated navigation system for the NAE Convair 580 research aircraft. | |
BEBENIN et al. | Equipment for cosmonaut EVA | |
AIYAMA | Active Efforts by Ourselves for the Development of Cryogenics! | |
Collins | Design for use, design for the millions; proposals and options of the National Industrial Design Council 1948-1960. | |
HUGUIER | Stabilization of satellites equipped with large solar panels | |
Heimlich et al. | Life support in the Shuttle Era | |
Ghmmam | An investigation into the effect of aerodynamic cross-coupling on aircraft motion at high angles of attack. | |
McCaffrey | Space Station/platform configurations | |
LEBEDINETS | Dust in the upper atmosphere and in space. Meteors(Russian book) | |
GIBB | Orbiter environmental control and life support system | |
HORAN et al. | Telemetry downlink interfaces and level-zero processing(Final Report, 1 Oct. 1988- 30 Sep. 1991) | |
TANABE et al. | New approach to spacecraft control system reconfiguration | |
BYSTROVA | Dust clouds in Orion and the interstellar neutral hydrogen distribution(Abstract Only) | |
POELAERT | Attitude stability criterion of deformable satellites(Attitude stability model for elastic and multispin stabilized spacecraft, based on energy dissipation) | |
SMITH | NASA Marshall Space Flight Center solar observatory(Report, Jan.- Mar. 1988) | |
REBROV | Krasnaya Zvezda on advantages of Cosmos-1443 modular spacecraft |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |