FR2833242A3 - Methodes et systemes pour diriger des satellites a energie de propulsion electrique pour les maintenir sur orbite stationnaire - Google Patents

Methodes et systemes pour diriger des satellites a energie de propulsion electrique pour les maintenir sur orbite stationnaire

Info

Publication number
FR2833242A3
FR2833242A3 FR0211943A FR0211943A FR2833242A3 FR 2833242 A3 FR2833242 A3 FR 2833242A3 FR 0211943 A FR0211943 A FR 0211943A FR 0211943 A FR0211943 A FR 0211943A FR 2833242 A3 FR2833242 A3 FR 2833242A3
Authority
FR
France
Prior art keywords
electric propulsion
systems
methods
keep
stationary orbit
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.)
Withdrawn
Application number
FR0211943A
Other languages
English (en)
Other versions
FR2833242A1 (fr
Inventor
Thomas Randolph
David Oh
Guenter Fischer
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.)
Maxar Space LLC
Original Assignee
Space Systems Loral LLC
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 Space Systems Loral LLC filed Critical Space Systems Loral LLC
Publication of FR2833242A3 publication Critical patent/FR2833242A3/fr
Publication of FR2833242A1 publication Critical patent/FR2833242A1/fr
Withdrawn legal-status Critical Current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
    • B64G1/22—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
    • 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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/405—Ion or plasma engines
    • 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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/411—Electric propulsion
    • B64G1/415—Arcjets or resistojets
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/428—Power distribution and management

Abstract

Méthodes et systèmes pour diriger des satellites à énergie de propulsion électrique pour les maintenir sur orbite stationnaire. Un dispositif à propulsion électrique (PE) est utilisé pour permettre à un satellite d'effectuer un trajet suivant une orbite terrestre stationnaire prédéterminée. La puissance propulsive et électrique du PE sont réglées pour faire varier la poussée et l'impulsion spécifique du dispositif PE. Un réseau solaire fournit l'énergie électrique pendant chaque cycle d'un jour terrestre avec un excès de puissance au-delà de celle nécessaire par l'engin spatial stockée dans une batterie. Une commande informatique gère la tension, le courant et la durée de fonctionnement pour minimiser la consommation d'énergie de propulsion et l'impact à l'égard du système.
FR0211943A 2001-10-15 2002-09-26 Methodes et systemes pour diriger des satellites a energie de propulsion electrique pour les maintenir sur orbite stationnaire Withdrawn FR2833242A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/977,834 US6581880B2 (en) 2001-10-15 2001-10-15 Energy managed electric propulsion methods and systems for stationkeeping satellites

Publications (2)

Publication Number Publication Date
FR2833242A3 true FR2833242A3 (fr) 2003-06-13
FR2833242A1 FR2833242A1 (fr) 2003-06-13

Family

ID=25525564

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0211943A Withdrawn FR2833242A1 (fr) 2001-10-15 2002-09-26 Methodes et systemes pour diriger des satellites a energie de propulsion electrique pour les maintenir sur orbite stationnaire

Country Status (3)

Country Link
US (1) US6581880B2 (fr)
JP (1) JP2003175900A (fr)
FR (1) FR2833242A1 (fr)

Families Citing this family (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20040149861A1 (en) * 2001-06-06 2004-08-05 Strobl William Charles S & H Cycle Engine
US20050133670A1 (en) * 2003-12-03 2005-06-23 Wang H. G. Unified sensor-based attitude determination and control for spacecraft operations
US7665695B2 (en) * 2003-12-03 2010-02-23 The Boeing Company Unified attitude control for spacecraft transfer orbit operations
GB2413861A (en) * 2004-05-06 2005-11-09 Vega Group Plc Controlling power to satellite electric propulsion system during eclipses.
US7922124B2 (en) 2006-12-07 2011-04-12 The Boeing Company Power optimized system for electric propulsion stationkeeping geosynchronous spacecraft
US8152108B2 (en) * 2008-06-17 2012-04-10 The Boeing Company Solar array peak power extraction
RU2483400C2 (ru) * 2011-06-17 2013-05-27 Федеральное Государственное Унитарное Предприятие "Государственный научно-производственный ракетно-космический центр "ЦСКБ-Прогресс" (ФГУП "ГНПРКЦ "ЦСКБ-Прогресс") Способ эксплуатации никель-водородных аккумуляторных батарей системы электропитания космического аппарата (варианты)
FR2986213B1 (fr) * 2012-02-01 2014-10-10 Snecma Engin spatial a propulsion electrique et chimique a propergol solide
US8915472B2 (en) 2012-05-11 2014-12-23 The Boeing Company Multiple space vehicle launch system
US9180984B2 (en) 2012-05-11 2015-11-10 The Boeing Company Methods and apparatus for performing propulsion operations using electric propulsion systems
FR3010053B1 (fr) * 2013-08-30 2016-10-21 Thales Sa Procede et dispositif de propulsion electrique de satellite
US10006445B2 (en) 2014-02-18 2018-06-26 The George Washington University Method and system for a programmable and fault tolerant pulsed plasma thruster
EP3218265A4 (fr) * 2014-11-13 2017-11-29 Aerojet Rocketdyne, Inc. Architecture de puissance pour applications de propulsion électrique solaire
US20160299179A1 (en) * 2015-04-13 2016-10-13 Mediatek Inc. Scheme capable of estimating available power range according to extra power range and employing available power range as reference of performing power throttling upon a system
CN106777638B (zh) * 2016-12-08 2020-06-26 上海宇航系统工程研究所 一种偏心航天器推进舱零配平布局设计方法
US11203447B1 (en) 2018-05-14 2021-12-21 United States Of America As Represented By The Secretary Of The Air Force Propulsion system for space vehicles
US11346306B1 (en) 2019-01-03 2022-05-31 Ball Aerospace & Technologies Corp. Chemical and cold gas propellant systems and methods
US11498705B1 (en) 2019-05-09 2022-11-15 Ball Aerospace & Technology Corp. On orbit fluid propellant dispensing systems and methods
FR3115769A1 (fr) * 2020-11-01 2022-05-06 Marc Grosman Vaisseau spatial équipé de propulseur à antimatière.
CN113738606B (zh) * 2021-08-27 2022-10-25 西安交通大学 一种针对离子电推进系统的连续变推力最优控制系统和方法
US11945606B1 (en) 2021-10-19 2024-04-02 Ball Aerospace & Technologies Corp. Electric propulsion based spacecraft propulsion systems and methods utilizing multiple propellants

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4825646A (en) * 1987-04-23 1989-05-02 Hughes Aircraft Company Spacecraft with modulated thrust electrostatic ion thruster and associated method
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.
US5267167A (en) * 1991-05-10 1993-11-30 Ball Corporation Method and system for formationfinding and formationkeeping in a constellation of satellites
US5595360A (en) * 1994-03-25 1997-01-21 Hughes Aircraft Company Optimal transfer orbit trajectory using electric propulsion
US5610820A (en) * 1995-03-23 1997-03-11 Martin Marietta Corp. Minimum propellant, zero momentum spacecraft attitude control system
US5810295A (en) * 1996-07-10 1998-09-22 Hughes Electronics Corporation Method and apparatus for a satellite station keeping
CN1235569A (zh) * 1996-11-01 1999-11-17 乔治·H·米利 利用惯性静电约束放电等离子体的等离子体喷射源
US5806804A (en) * 1996-11-12 1998-09-15 Lockheed Martin Corp. Adaptive harmonic disturbance compensation system
US5947421A (en) * 1997-07-09 1999-09-07 Beattie; John R. Electrostatic propulsion systems and methods
US6036143A (en) * 1997-12-18 2000-03-14 Trw Inc. Solar array-mounted stationkeeping and maneuvering thrusters
US6032904A (en) * 1998-02-23 2000-03-07 Space Systems/Loral, Inc. Multiple usage thruster mounting configuration
US6089508A (en) * 1998-03-02 2000-07-18 Hughes Electronics Corporation Autonomous spacecraft safing with reaction wheels
US6027076A (en) * 1998-07-09 2000-02-22 Hughes Electronics Corporation Method for powering a spacecraft with extended-life battery operation
US6341749B1 (en) * 1998-09-25 2002-01-29 Hughes Electronics Corporation Method of simultaneously reducing inclination and eccentricity for geostationary orbit transfer
US6260805B1 (en) * 1998-12-29 2001-07-17 Hughes Electronics Corporation Method of controlling attitude of a momentum biased spacecraft during long-duration thruster firings
US6186446B1 (en) * 1999-06-08 2001-02-13 Space Systems/Loral, Inc. Solar array control for electric propulsion system

Also Published As

Publication number Publication date
FR2833242A1 (fr) 2003-06-13
US20030075645A1 (en) 2003-04-24
US6581880B2 (en) 2003-06-24
JP2003175900A (ja) 2003-06-24

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