DE69423094D1 - Optimale Transferbahntrajektorie mit elektrischem Triebwerk - Google Patents

Optimale Transferbahntrajektorie mit elektrischem Triebwerk

Info

Publication number
DE69423094D1
DE69423094D1 DE69423094T DE69423094T DE69423094D1 DE 69423094 D1 DE69423094 D1 DE 69423094D1 DE 69423094 T DE69423094 T DE 69423094T DE 69423094 T DE69423094 T DE 69423094T DE 69423094 D1 DE69423094 D1 DE 69423094D1
Authority
DE
Germany
Prior art keywords
transfer path
electric engine
optimal transfer
path trajectory
trajectory
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 - Lifetime
Application number
DE69423094T
Other languages
English (en)
Other versions
DE69423094T2 (de
Inventor
Arnon Spitzer
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.)
DirecTV Group Inc
Original Assignee
Hughes Electronics Corp
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 Hughes Electronics Corp filed Critical Hughes Electronics Corp
Application granted granted Critical
Publication of DE69423094D1 publication Critical patent/DE69423094D1/de
Publication of DE69423094T2 publication Critical patent/DE69423094T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • B64G1/242—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
    • 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
    • B64G1/002—Launch 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
    • B64G1/40—Arrangements or adaptations of propulsion systems
    • B64G1/411—Electric propulsion
    • B64G1/415—Arcjets or resistojets
DE69423094T 1994-03-25 1994-12-27 Optimale Transferbahntrajektorie mit elektrischem Triebwerk Expired - Lifetime DE69423094T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/217,791 US5595360A (en) 1994-03-25 1994-03-25 Optimal transfer orbit trajectory using electric propulsion

Publications (2)

Publication Number Publication Date
DE69423094D1 true DE69423094D1 (de) 2000-03-30
DE69423094T2 DE69423094T2 (de) 2000-06-21

Family

ID=22812537

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69423094T Expired - Lifetime DE69423094T2 (de) 1994-03-25 1994-12-27 Optimale Transferbahntrajektorie mit elektrischem Triebwerk

Country Status (4)

Country Link
US (2) US5595360A (de)
EP (1) EP0673833B1 (de)
CN (1) CN1093949C (de)
DE (1) DE69423094T2 (de)

Families Citing this family (76)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6102337A (en) * 1995-12-22 2000-08-15 Hughes Electronics Corporation Spacecraft attitude control with gimbaled thrusters
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
FR2757825B1 (fr) * 1996-12-31 1999-03-26 Europ Propulsion Procede et systeme de lancement simultane de satellites sur des orbites non coplanaires en utilisant des orbites tres excentriques et du freinage atmospherique
WO1998033704A2 (en) 1997-02-04 1998-08-06 Belbruno Edward A Computer implemented procedure for ballistic capture transfer
US6097997A (en) * 1997-03-25 2000-08-01 Galaxy Development, Llc Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same
AU7357198A (en) 1997-03-25 1998-10-20 Edward A. Belbruno Low energy method for changing the inclinations of orbiting satellites using weak stability boundaries and a computer process for implementing same
CN1086988C (zh) * 1997-04-24 2002-07-03 银河系发展公司 利用弱稳定边界改变飞行物体倾角和/或高度的方法
FR2768399B1 (fr) * 1997-09-12 1999-11-12 Aerospatiale Procede de mise sur orbite geostationnaire d'un satellite artificiel
US6116545A (en) * 1998-04-09 2000-09-12 Hughes Electronics Corporation Free return lunar flyby transfer method for geosynchronous satellites
US6149103A (en) * 1998-04-09 2000-11-21 Hughes Electronics Corporation Free return lunar flyby transfer method for geosynchronous satellites havint multiple perilune stages
US6128575A (en) * 1998-06-10 2000-10-03 Hughes Electrnoics Corporation Methods for accurately inserting satellite constellations into common orbit planes
US6341749B1 (en) * 1998-09-25 2002-01-29 Hughes Electronics Corporation Method of simultaneously reducing inclination and eccentricity for geostationary orbit transfer
US6135394A (en) * 1998-12-08 2000-10-24 Space Systems/Loral, Inc. Practical method and apparatus for satellite stationkeeping
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
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
US6385512B1 (en) 1999-04-16 2002-05-07 Galaxy Development Llc System and method of a ballistic capture transfer to L4, L5
US6186446B1 (en) 1999-06-08 2001-02-13 Space Systems/Loral, Inc. Solar array control for electric propulsion system
US7113851B1 (en) * 1999-06-09 2006-09-26 Walter Gelon Practical orbit raising system and method for geosynchronous satellites
US6464174B1 (en) * 2000-06-21 2002-10-15 Space Systems/Loral, Inc. Round-trip orbital operation of a spacecraft
US6237876B1 (en) * 2000-07-28 2001-05-29 Space Systems/Loral, Inc. Methods for using satellite state vector prediction to provide three-axis satellite attitude control
US6739555B2 (en) 2001-08-03 2004-05-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Reusable module for the storage, transportation, and supply of multiple propellants in a space environment
US6543723B1 (en) * 2001-09-04 2003-04-08 Space Systems/Loral, Inc. Electric orbit raising with variable thrust
US6581880B2 (en) * 2001-10-15 2003-06-24 Space Systems/Loral, Inc. Energy managed electric propulsion methods and systems for stationkeeping satellites
US20050109878A1 (en) * 2002-03-28 2005-05-26 Dutch Space B.V. Spacecraft and method for building such a spacecraft and an adapter to be used in such a spacecraft
US6672542B2 (en) * 2002-06-03 2004-01-06 The Aerospace Corporation Method and system for controlling the eccentricity of a near-circular orbit
JP4488707B2 (ja) * 2003-09-26 2010-06-23 富士通株式会社 人工衛星の軌道制御計画方法、プログラム及び装置
US7832687B1 (en) 2004-08-24 2010-11-16 Lockheed Martin Corporation On-orbit storage, plane change, and injection to final orbit of space vehicles
JP5119514B2 (ja) * 2008-01-09 2013-01-16 独立行政法人 宇宙航空研究開発機構 イオン噴射装置、推進装置及び人工衛星
CN101539483B (zh) * 2009-04-29 2010-11-03 北京航空航天大学 电推进试验平台测量控制装置
US20120119034A1 (en) * 2009-07-02 2012-05-17 Space Systems/Loral, Inc. Deorbiting a Spacecraft from a Highly Inclined Elliptical Orbit
FR2955313B1 (fr) * 2010-01-19 2012-11-16 Thales Sa Procede et dispositif d'optimisation de la masse d'un satellite
US9108748B2 (en) * 2010-10-20 2015-08-18 Space Systems/Loral, Llc Satellite orbit raising using electric propulsion
US9108749B2 (en) * 2010-10-20 2015-08-18 Space Systems/Loral, Llc Spacecraft momentum management
US8930048B1 (en) 2011-04-14 2015-01-06 The Boeing Company Enhanced compound steering law for general low thrust mission
US8457810B1 (en) 2011-04-14 2013-06-04 The Boeing Company Compound steering law for efficient low thrust transfer orbit trajectory
RU2487823C1 (ru) * 2011-12-08 2013-07-20 Открытое акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" Способ адаптивного управления движением центра масс космического аппарата
US9180984B2 (en) * 2012-05-11 2015-11-10 The Boeing Company Methods and apparatus for performing propulsion operations using electric propulsion systems
US8915472B2 (en) * 2012-05-11 2014-12-23 The Boeing Company Multiple space vehicle launch system
US8763957B1 (en) * 2012-10-08 2014-07-01 Space Systems/Loral, Llc Spacecraft transfer orbit techniques
FR2998875B1 (fr) * 2012-11-30 2015-07-17 Thales Sa Procede et systeme de mise a poste d'un satellite
CA2831309C (en) * 2012-12-04 2017-05-30 The Boeing Company Methods and apparatus for performing propulsion operations using electric propulsion systems
FR3014082B1 (fr) * 2013-11-29 2016-01-01 Thales Sa Systeme de tuyeres et procede pour le controle d'orbite et d'attitude pour satellite geostationnaire
FR3018121B1 (fr) * 2014-02-28 2016-02-12 Thales Sa Procede de suivi d'une orbite de transfert ou d'une phase de mise en orbite d'un vehicule spatial, en particulier a propulsion electrique, et appareil pour la mise en oeuvre d'un tel procede
US10444371B2 (en) * 2014-03-21 2019-10-15 The Boeing Company Interference geolocation using a satellite constellation
US9284068B2 (en) * 2014-04-08 2016-03-15 The Boeing Company Fast-low energy transfer to Earth-Moon Lagrange point L2
RU2586945C2 (ru) * 2014-07-07 2016-06-10 Акционерное общество "Информационные спутниковые системы" имени академика М.Ф. Решетнёва" Способ выведения космического аппарата на геостационарную орбиту с использованием двигателей малой тяги
FR3024128B1 (fr) * 2014-07-25 2016-07-22 Thales Sa Procede de mise a poste d'un satellite et de test en orbite de sa charge utile
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
CN105005643B (zh) * 2015-06-26 2018-01-23 北京航空航天大学 一种载人登月质量规模估算的方法与系统
US9764859B2 (en) * 2015-06-29 2017-09-19 The Boeing Company Efficient stationkeeping design for mixed fuel systems
US10005568B2 (en) 2015-11-13 2018-06-26 The Boeing Company Energy efficient satellite maneuvering
CN105607478B (zh) * 2016-01-21 2017-07-07 北京理工大学 地球静止轨道航天器电推进转移轨道控制方法
US10144531B2 (en) * 2016-02-04 2018-12-04 The Boeing Company Reorientation of a spinning spacecraft using gimbaled electric thrusters
US11267588B2 (en) * 2016-04-29 2022-03-08 Quicklaunch, Inc. Orbital mechanics of impulsive launch
US10427804B1 (en) * 2016-04-29 2019-10-01 Quicklaunch, Inc. Orbital mechanics of impulsive launch
US10084536B1 (en) * 2016-08-25 2018-09-25 Star Mesh LLC Radio system using satellites
US10464694B1 (en) 2017-03-23 2019-11-05 Space Systems/Loral, Llc Asymmetric thruster gimbal configuration
US10435183B1 (en) 2017-04-14 2019-10-08 Space Systems/Loral, Llc Deployable propulsion module for spacecraft
US10085200B1 (en) 2017-09-29 2018-09-25 Star Mesh LLC Radio system using nodes with high gain antennas
US10291316B1 (en) 2017-12-11 2019-05-14 Star Mesh LLC Data transmission systems and methods using satellite-to-satellite radio links
US11155368B1 (en) 2018-03-13 2021-10-26 Space Systems/Loral, Llc Multiple thruster firing on a single articulable module
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
AU2019301682A1 (en) 2018-07-12 2021-01-21 Star Mesh LLC Communications systems and methods with stochastically distributed orbiting satellites
CN109460049B (zh) * 2018-11-14 2021-11-16 北京控制工程研究所 基于惯性指向模式的地球同步轨道卫星远地点变轨方法
US11401053B2 (en) * 2018-12-20 2022-08-02 The Boeing Company Autonomous control of electric power supplied to a thruster during electric orbit raising
US11396388B2 (en) * 2018-12-20 2022-07-26 The Boeing Company Optimized power balanced variable thrust transfer orbits to minimize an electric orbit raising duration
US11753188B2 (en) * 2018-12-20 2023-09-12 The Boeing Company Optimized power balanced low thrust transfer orbits utilizing split thruster execution
CN109739262B (zh) * 2019-01-25 2022-04-19 上海微小卫星工程中心 一种快速自主转移轨道控制方法
US11377237B1 (en) 2019-05-01 2022-07-05 United Launch Alliance, L.L.C. Orbital rendezvous techniques
US11870543B2 (en) 2020-05-18 2024-01-09 Star Mesh LLC Data transmission systems and methods for low earth orbit satellite communications
FR3110549A1 (fr) 2020-05-19 2021-11-26 Airbus Defence And Space Sas Procédé d’optimisation du transfert d’orbite d’un engin spatial à propulsion électrique et satellite mettant en œuvre ledit procédé
CN111891393B (zh) * 2020-08-11 2022-03-15 中国科学院微小卫星创新研究院 小型高轨卫星公用平台的混合推进舱
CN114313309B (zh) * 2020-08-12 2023-08-04 中国科学院微小卫星创新研究院 小型高轨卫星的自主变轨方法
CN113899257B (zh) * 2021-08-23 2023-04-14 上海宇航系统工程研究所 一种基于迭代制导的运载火箭轨道参数重构方法
CN113928598A (zh) * 2021-12-16 2022-01-14 亚太卫星宽带通信（深圳）有限公司 一种实现同步轨道卫星漂星的方法及装置
CN115682919B (zh) * 2022-10-28 2023-08-11 哈尔滨工业大学 一种基于曲面积分的霍尔推力器推力矢量偏心计算方法

Family Cites Families (4)

* 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
US4943014A (en) * 1979-10-30 1990-07-24 Trw Inc. Soft ride method for changing the altitude or position of a spacecraft in orbit
FR2491867A1 (fr) * 1980-09-02 1982-04-16 Aerospatiale Procede de changement d'orbite d'un satellite, notamment d'injection en orbite geostationnaire et satellite mettant en oeuvre ledit procede
US4741502A (en) * 1985-10-01 1988-05-03 Hughes Aircraft Company Method and apparatus for launching a spacecraft by use of a recoverable upper rocket stage

Also Published As

Publication number Publication date
US5716029A (en) 1998-02-10
EP0673833A1 (de) 1995-09-27
EP0673833B1 (de) 2000-02-23
DE69423094T2 (de) 2000-06-21
US5595360A (en) 1997-01-21
CN1093949C (zh) 2002-11-06
CN1131291A (zh) 1996-09-18

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