DE69730110D1 - Verfahren um Satelliten in nicht-koplanare Umlaufbahnen unter Verwendung von sehr excentrischen Umlaufbahnen und atmosphärischem Strömungswiderstand gleichzeitig zu bringen - Google Patents

Verfahren um Satelliten in nicht-koplanare Umlaufbahnen unter Verwendung von sehr excentrischen Umlaufbahnen und atmosphärischem Strömungswiderstand gleichzeitig zu bringen

Info

Publication number
DE69730110D1
DE69730110D1 DE69730110T DE69730110T DE69730110D1 DE 69730110 D1 DE69730110 D1 DE 69730110D1 DE 69730110 T DE69730110 T DE 69730110T DE 69730110 T DE69730110 T DE 69730110T DE 69730110 D1 DE69730110 D1 DE 69730110D1
Authority
DE
Germany
Prior art keywords
orbits
satellites
bring
coplanar
eccentric
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
Application number
DE69730110T
Other languages
English (en)
Other versions
DE69730110T2 (de
Inventor
Christophe Koppel
Dominique Valentian
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
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
Application filed by Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of DE69730110D1 publication Critical patent/DE69730110D1/de
Publication of DE69730110T2 publication Critical patent/DE69730110T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00—Cosmonautic vehicles
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1085—Swarms and constellations
    • 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
    • B64G1/002—Launch systems
DE69730110T 1996-12-31 1997-12-22 Verfahren um Satelliten in nicht-koplanare Umlaufbahnen unter Verwendung von sehr excentrischen Umlaufbahnen und atmosphärischem Strömungswiderstand gleichzeitig zu bringen Expired - Fee Related DE69730110T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR9616276 1996-12-31
FR9616276A FR2757825B1 (fr) 1996-12-31 1996-12-31 Procede et systeme de lancement simultane de satellites sur des orbites non coplanaires en utilisant des orbites tres excentriques et du freinage atmospherique

Publications (2)

Publication Number Publication Date
DE69730110D1 true DE69730110D1 (de) 2004-09-09
DE69730110T2 DE69730110T2 (de) 2004-12-09

Family

ID=9499352

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69730110T Expired - Fee Related DE69730110T2 (de) 1996-12-31 1997-12-22 Verfahren um Satelliten in nicht-koplanare Umlaufbahnen unter Verwendung von sehr excentrischen Umlaufbahnen und atmosphärischem Strömungswiderstand gleichzeitig zu bringen

Country Status (7)

Country Link
US (1) US5961077A (de)
EP (1) EP0854083B1 (de)
JP (1) JPH1179100A (de)
CN (1) CN1083787C (de)
DE (1) DE69730110T2 (de)
FR (1) FR2757825B1 (de)
RU (1) RU2220886C2 (de)

Families Citing this family (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6843446B2 (en) * 1993-11-12 2005-01-18 David D. Scott Apparatus and methods for in-space satellite operations
US6257526B1 (en) 1998-11-09 2001-07-10 Hughes Electronics Corporation Satellite system and method of deploying same
US6327523B2 (en) 1999-01-21 2001-12-04 Hughes Electronics Corporation Overhead system of inclined eccentric geosynchronous orbitting satellites
US6364252B1 (en) * 1999-03-11 2002-04-02 Constellation Services International, Inc. Method of using dwell times in intermediate orbits to optimize orbital transfers and method and apparatus for satellite repair
US20020130222A1 (en) * 1999-03-11 2002-09-19 Constellation Services International Method of using dwell times in intermediate orbits to optimize orbital transfers and method and apparatus for satellite repair
US6453220B1 (en) * 2000-01-31 2002-09-17 Space Systems/Loral, Inc. Low earth orbit satellite constellation stationkeeping algorithm with absolute altitude control
US7184761B1 (en) * 2000-03-27 2007-02-27 The Directv Group, Inc. Satellite communications system
US7369809B1 (en) 2000-10-30 2008-05-06 The Directv Group, Inc. System and method for continuous broadcast service from non-geostationary orbits
US6830222B1 (en) 2002-03-21 2004-12-14 Global Aerospace Corporation Balloon device for lowering space object orbits
US7832687B1 (en) 2004-08-24 2010-11-16 Lockheed Martin Corporation On-orbit storage, plane change, and injection to final orbit of space vehicles
US7689358B2 (en) * 2006-04-25 2010-03-30 Northrop Grumman Corporation Delta-V-free satellite cloud cluster flying
FR2982045B1 (fr) * 2011-10-28 2013-12-27 Thales Sa Procede et systeme de commande d'un ensemble d'au moins deux satellites adaptes pour fournir un service
US8655589B2 (en) * 2012-01-25 2014-02-18 Mitsubishi Electric Research Laboratories, Inc. System and method for controlling motion of spacecrafts
US9114893B2 (en) * 2012-07-26 2015-08-25 Mitsubishi Electric Research Laboratories, Inc. System and method for estimating states of spacecraft in planet-moon environment
US8768622B2 (en) * 2012-09-14 2014-07-01 The United States Of America, As Represented By The Secretary Of The Navy System and method for maneuver plan for satellites flying in proximity using apocentral coordinate system
CN103072701B (zh) * 2013-01-30 2013-10-16 北京控制工程研究所 一种欠驱动的卫星消旋控制方法
CN103072703B (zh) * 2013-01-30 2013-10-16 北京控制工程研究所 一种欠驱动的卫星进动控制方法
US9284068B2 (en) * 2014-04-08 2016-03-15 The Boeing Company Fast-low energy transfer to Earth-Moon Lagrange point L2
FR3020348B1 (fr) 2014-04-24 2016-05-13 Snecma Procede de deploiement d'une constellation de satellites
CN104354880B (zh) * 2014-10-17 2016-08-17 北京航空航天大学 一种用于空间姿态调整的双偏心盘装置
RU2583507C1 (ru) * 2015-02-05 2016-05-10 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Способ одновременного выведения группы спутников на некомпланарные орбиты (варианты)
US10009101B2 (en) 2015-03-17 2018-06-26 The Boeing Company Laser communications following an atmospheric event
US10313010B2 (en) * 2015-03-17 2019-06-04 The Boeing Company Laser communications in super-geosynchronous earth orbit
RU2605463C2 (ru) * 2015-04-03 2016-12-20 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ управления транспортной космической системой
US9919813B2 (en) 2015-04-15 2018-03-20 The United States Of America, As Represented By The Secretary Of The Navy Control system and method for a plane change for satellite operations
JP6542581B2 (ja) * 2015-05-19 2019-07-10 株式会社Ｉｈｉエアロスペース 宇宙機とその軌道面変更方法
RU2614466C2 (ru) * 2015-07-20 2017-03-28 Открытое акционерное общество "Ракетно-космическая корпорация "Энергия" имени С.П. Королева" Способ управления транспортной космической системой
RU2643082C1 (ru) * 2016-02-29 2018-01-30 Акционерное общество "Военно-промышленная корпорация "Научно-производственное объединение машиностроения" Многоцелевая трансформируемая орбитальная система и способ ее применения
US10427804B1 (en) * 2016-04-29 2019-10-01 Quicklaunch, Inc. Orbital mechanics of impulsive launch
US11267588B2 (en) * 2016-04-29 2022-03-08 Quicklaunch, Inc. Orbital mechanics of impulsive launch
US10053241B2 (en) * 2016-12-01 2018-08-21 The Boeing Company Systems and methods for multi-spacecraft distributed ascent
CN109539903B (zh) * 2018-10-31 2020-10-16 湖北航天技术研究院总体设计所 一种固体运载火箭椭圆转移轨道迭代制导控制方法
CN110104219B (zh) * 2019-04-24 2020-09-08 中国人民解放军63920部队 一种控制探测器着陆地外天体的方法及装置
CN110543676B (zh) * 2019-07-31 2023-01-24 中南大学 一种基于代理模型的卫星集群构形重构规划方法及系统
KR102464559B1 (ko) * 2021-04-14 2022-11-09 한국항공우주연구원 궤도 천이 장치
CN114313313B (zh) * 2021-12-09 2023-02-28 哈尔滨工业大学 全电推进小卫星初始布轨至圆轨道的方法、装置及介质

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3907225A (en) * 1973-12-17 1975-09-23 Tru Inc Spacecraft for deploying objects into selected flight paths
US4504031A (en) * 1979-11-01 1985-03-12 The Boeing Company Aerodynamic braking and recovery method for a space vehicle
US5199672A (en) * 1990-05-25 1993-04-06 Orbital Sciences Corporation Method and apparatus for deploying a satellite network
US5393017A (en) * 1993-01-25 1995-02-28 Lockheed Missiles & Space Company, Inc. Technique for dispensing earth satellites into multi-planar orbits
US5681011A (en) * 1993-08-24 1997-10-28 Orbital Sciences Corporation Method for injecting payloads into orbit
US5595360A (en) * 1994-03-25 1997-01-21 Hughes Aircraft Company Optimal transfer orbit trajectory using electric propulsion

Also Published As

Publication number Publication date
DE69730110T2 (de) 2004-12-09
RU2220886C2 (ru) 2004-01-10
FR2757825A1 (fr) 1998-07-03
EP0854083A1 (de) 1998-07-22
JPH1179100A (ja) 1999-03-23
CN1195630A (zh) 1998-10-14
US5961077A (en) 1999-10-05
FR2757825B1 (fr) 1999-03-26
CN1083787C (zh) 2002-05-01
EP0854083B1 (de) 2004-08-04

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8339 Ceased/non-payment of the annual fee