DE3168786D1 - Method of changing the orbit of a satellite, especially for injection in a geosynchronous orbit, and satellite using this method - Google Patents
Method of changing the orbit of a satellite, especially for injection in a geosynchronous orbit, and satellite using this methodInfo
- Publication number
- DE3168786D1 DE3168786D1 DE8181401354T DE3168786T DE3168786D1 DE 3168786 D1 DE3168786 D1 DE 3168786D1 DE 8181401354 T DE8181401354 T DE 8181401354T DE 3168786 T DE3168786 T DE 3168786T DE 3168786 D1 DE3168786 D1 DE 3168786D1
- Authority
- DE
- Germany
- Prior art keywords
- satellite
- orbit
- injection
- changing
- geosynchronous
- 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
Links
- 238000000034 method Methods 0.000 title 2
- 238000002347 injection Methods 0.000 title 1
- 239000007924 injection Substances 0.000 title 1
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
- B64G1/242—Orbits and trajectories
- B64G1/2427—Transfer orbits
-
- 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
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8018918A FR2491867A1 (fr) | 1980-09-02 | 1980-09-02 | Procede de changement d'orbite d'un satellite, notamment d'injection en orbite geostationnaire et satellite mettant en oeuvre ledit procede |
Publications (1)
Publication Number | Publication Date |
---|---|
DE3168786D1 true DE3168786D1 (en) | 1985-03-21 |
Family
ID=9245564
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE8181401354T Expired DE3168786D1 (en) | 1980-09-02 | 1981-08-27 | Method of changing the orbit of a satellite, especially for injection in a geosynchronous orbit, and satellite using this method |
Country Status (4)
Country | Link |
---|---|
EP (1) | EP0047211B1 (de) |
JP (1) | JPS5777298A (de) |
DE (1) | DE3168786D1 (de) |
FR (1) | FR2491867A1 (de) |
Families Citing this family (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5595360A (en) * | 1994-03-25 | 1997-01-21 | Hughes Aircraft Company | Optimal transfer orbit trajectory using electric propulsion |
FR2747102B1 (fr) * | 1996-04-05 | 1998-06-26 | Europ Propulsion | Procede et systeme de mise en orbite d'un vehicule spatial avec des propulseurs a forte impulsion specifique |
US6341749B1 (en) * | 1998-09-25 | 2002-01-29 | Hughes Electronics Corporation | Method of simultaneously reducing inclination and eccentricity for geostationary orbit transfer |
US6672542B2 (en) * | 2002-06-03 | 2004-01-06 | The Aerospace Corporation | Method and system for controlling the eccentricity of a near-circular orbit |
CN114348298B (zh) * | 2021-11-30 | 2023-05-16 | 中国西安卫星测控中心 | 适用于地球同步卫星混合推进入轨的联合优化方法 |
CN115535307B (zh) * | 2022-12-01 | 2023-03-03 | 银河航天(北京)通信技术有限公司 | 卫星轨道转移策略确定方法以及装置 |
CN116461721A (zh) * | 2023-05-15 | 2023-07-21 | 中国科学院微小卫星创新研究院 | 一种应用于卫星辅助入轨的模块化电磁动力背包及卫星入轨方法 |
Family Cites Families (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2569162A1 (fr) * | 1977-11-25 | 1986-02-21 | Ford Aerospace & Communication | Procede de mise sur orbite de satellites et de vaisseaux spatiaux |
-
1980
- 1980-09-02 FR FR8018918A patent/FR2491867A1/fr active Granted
-
1981
- 1981-08-27 DE DE8181401354T patent/DE3168786D1/de not_active Expired
- 1981-08-27 EP EP81401354A patent/EP0047211B1/de not_active Expired
- 1981-08-31 JP JP56136943A patent/JPS5777298A/ja active Granted
Also Published As
Publication number | Publication date |
---|---|
FR2491867A1 (fr) | 1982-04-16 |
FR2491867B1 (de) | 1982-11-12 |
EP0047211B1 (de) | 1985-02-06 |
EP0047211A1 (de) | 1982-03-10 |
JPH0215440B2 (de) | 1990-04-12 |
JPS5777298A (en) | 1982-05-14 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8363 | Opposition against the patent | ||
8331 | Complete revocation |