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 method

Info

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
Application number
DE8181401354T
Other languages
German (de)
English (en)
Inventor
Andre Mortelette
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=9245564&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE3168786(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of DE3168786D1 publication Critical patent/DE3168786D1/de
Expired legal-status Critical Current

Links

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)
DE8181401354T 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 Expired DE3168786D1 (en)

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 (Direct)
JP (1) JPS5777298A (Direct)
DE (1) DE3168786D1 (Direct)
FR (1) FR2491867A1 (Direct)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
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
CN116461721B (zh) * 2023-05-15 2025-04-18 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
CN117125271B (zh) * 2023-09-04 2025-12-02 上海卫星工程研究所 大椭圆冻结轨道入轨方法和系统

Family Cites Families (1)

* Cited by examiner, † Cited by third party
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

Also Published As

Publication number Publication date
EP0047211A1 (fr) 1982-03-10
JPH0215440B2 (Direct) 1990-04-12
JPS5777298A (en) 1982-05-14
EP0047211B1 (fr) 1985-02-06
FR2491867A1 (fr) 1982-04-16
FR2491867B1 (Direct) 1982-11-12

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Legal Events

Date Code Title Description
8363 Opposition against the patent
8331 Complete revocation