ATE53551T1 - In zwei alternativen flugweisen operierendes raumfahrzeug. - Google Patents
In zwei alternativen flugweisen operierendes raumfahrzeug.Info
- Publication number
- ATE53551T1 ATE53551T1 AT86301554T AT86301554T ATE53551T1 AT E53551 T1 ATE53551 T1 AT E53551T1 AT 86301554 T AT86301554 T AT 86301554T AT 86301554 T AT86301554 T AT 86301554T AT E53551 T1 ATE53551 T1 AT E53551T1
- Authority
- AT
- Austria
- Prior art keywords
- spacecraft
- oriented
- control means
- flight modes
- alternative flight
- Prior art date
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 (2)
| 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 |
| EP86301554A EP0195553B1 (de) | 1985-03-20 | 1986-03-05 | In zwei alternativen Flugweisen operierendes Raumfahrzeug |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| ATE53551T1 true ATE53551T1 (de) | 1990-06-15 |
Family
ID=24867657
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| AT86301554T ATE53551T1 (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 (41)
| 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 |
| US5152482A (en) * | 1990-06-29 | 1992-10-06 | Standard Space Platforms Corp. | Modular mother satellite bus for subsidiary payloads |
| US5271582A (en) * | 1990-06-29 | 1993-12-21 | 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 |
| AU5572499A (en) * | 1998-08-19 | 2000-03-14 | 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 |
| RU2247684C2 (ru) * | 2003-03-25 | 2005-03-10 | Федеральное государственное унитарное предприятие "Государственный космический научно-производственный центр им. М.В. Хруничева" | Способ трехосной ориентации космического аппарата в орбитальной системе координат |
| US7823836B2 (en) * | 2006-12-04 | 2010-11-02 | The Boeing Company | Optimal sun safe attitude for satellite ground tracking |
| RU2412873C1 (ru) * | 2009-11-02 | 2011-02-27 | Федеральное Государственное унитарное предприятие Государственный научно-производственный ракетно-космический центр (ФГУП ГНПРКЦ "ЦСКБ-Прогресс") | Способ ориентации целевой аппаратуры космических аппаратов и устройство, его реализующее |
| 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 |
| EP3468868B1 (de) * | 2016-06-14 | 2021-05-19 | Blomquist, Richard | Raumfahrzeug und steuerungsverfahren |
| EP4234415A1 (de) * | 2017-09-10 | 2023-08-30 | Orbit Fab, Inc. | Systeme und verfahren zum zuführen, speichern und verarbeiten von materialien im raum |
| 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 |
| US3480232A (en) * | 1965-11-22 | 1969-11-25 | Us Navy | Damping coupler for satellite attitude control |
| US3362656A (en) * | 1965-11-22 | 1968-01-09 | Navy Usa | 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 |
| US3540676A (en) * | 1968-12-20 | 1970-11-17 | Nasa | Redundant actuating mechanism |
| US3567155A (en) * | 1968-12-20 | 1971-03-02 | James A Gatlin | Gravity gradient attitude control system |
| 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 DE DE8686301554T patent/DE3671875D1/de 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
- 1986-03-20 JP JP61063856A patent/JPS61268600A/ja active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPH0583440B2 (de) | 1993-11-26 |
| CA1326655C (en) | 1994-02-01 |
| EP0195553B1 (de) | 1990-06-13 |
| DE3671875D1 (de) | 1990-07-19 |
| JPS61268600A (ja) | 1986-11-28 |
| EP0195553A2 (de) | 1986-09-24 |
| US4728061A (en) | 1988-03-01 |
| EP0195553A3 (en) | 1987-09-16 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |