ATE460680T1 - Vorrichtung zur regelung der relativen positionen von einer gruppe in formation fliegender raumschiffe durch analyse von zweifrequenzsignalen - Google Patents

Vorrichtung zur regelung der relativen positionen von einer gruppe in formation fliegender raumschiffe durch analyse von zweifrequenzsignalen

Info

Publication number
ATE460680T1
ATE460680T1 AT06300040T AT06300040T ATE460680T1 AT E460680 T1 ATE460680 T1 AT E460680T1 AT 06300040 T AT06300040 T AT 06300040T AT 06300040 T AT06300040 T AT 06300040T AT E460680 T1 ATE460680 T1 AT E460680T1
Authority
AT
Austria
Prior art keywords
frequency signals
spaceships
flying
formation
controlling
Prior art date
Application number
AT06300040T
Other languages
English (en)
Inventor
Christian Mehlen
Estelle Pierre
Original Assignee
Thales Sa
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 Thales Sa filed Critical Thales Sa
Application granted granted Critical
Publication of ATE460680T1 publication Critical patent/ATE460680T1/de

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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • 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
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/0009—Transmission of position information to remote stations
    • G01S5/0072—Transmission between mobile stations, e.g. anti-collision systems
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
    • G01S5/0247—Determining attitude
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01S—RADIO DIRECTION-FINDING; RADIO NAVIGATION; DETERMINING DISTANCE OR VELOCITY BY USE OF RADIO WAVES; LOCATING OR PRESENCE-DETECTING BY USE OF THE REFLECTION OR RERADIATION OF RADIO WAVES; ANALOGOUS ARRANGEMENTS USING OTHER WAVES
    • G01S5/00—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations
    • G01S5/02—Position-fixing by co-ordinating two or more direction or position line determinations; Position-fixing by co-ordinating two or more distance determinations using radio waves
    • G01S5/0284—Relative positioning
AT06300040T 2006-01-19 2006-01-19 Vorrichtung zur regelung der relativen positionen von einer gruppe in formation fliegender raumschiffe durch analyse von zweifrequenzsignalen ATE460680T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
EP06300040A EP1813957B1 (de) 2006-01-19 2006-01-19 Vorrichtung zur Regelung der relativen Positionen von einer Gruppe in Formation fliegender Raumschiffe durch Analyse von Zweifrequenzsignalen

Publications (1)

Publication Number Publication Date
ATE460680T1 true ATE460680T1 (de) 2010-03-15

Family

ID=36579413

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06300040T ATE460680T1 (de) 2006-01-19 2006-01-19 Vorrichtung zur regelung der relativen positionen von einer gruppe in formation fliegender raumschiffe durch analyse von zweifrequenzsignalen

Country Status (9)

Country Link
US (1) US8463467B2 (de)
EP (1) EP1813957B1 (de)
JP (1) JP5007467B2 (de)
CN (1) CN101375176B (de)
AT (1) ATE460680T1 (de)
DE (1) DE602006012795D1 (de)
ES (1) ES2340062T3 (de)
RU (1) RU2419807C2 (de)
WO (1) WO2007082929A1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1986018B1 (de) * 2007-04-27 2014-11-19 Thales Alenia Space Italia S.p.A. Positions- und Richtungserkennung
US8965680B2 (en) 2011-02-25 2015-02-24 Honeywell International Inc. Systems and methods for providing improved TCAS bearing measurement
FR2976087B1 (fr) * 2011-06-01 2019-07-12 Thales Systeme de localisation geographique d'un emetteur de signaux radioelectriques situee a la surface de la terre, et procede associe d'interferometrie distribuee
CN102981175B (zh) * 2012-12-24 2014-04-30 北京理工大学 一种集群空间机器人主从式目标协同定位方法
RU2537818C1 (ru) * 2013-07-16 2015-01-10 Открытое акционерное общество "Российская корпорация ракетно-космического приборостроения и информационных систем" (ОАО "Российские космические системы") Способ коррекции траектории полета космического аппарата и устройство для его реализации
FR3017213B1 (fr) 2014-01-31 2016-02-05 Thales Sa Procede et systeme radiofrequence de determination, par couple d'engins spatiaux, de la position angulaire relative entre plusieurs engins spatiaux distants
TWI534453B (zh) * 2014-02-18 2016-05-21 原相科技股份有限公司 相對位置定位系統與追蹤系統
CN106094862A (zh) * 2016-06-22 2016-11-09 陕西宝成航空仪表有限责任公司 无人机编队飞行通信控制的实现方法
DE102017102481A1 (de) * 2017-02-08 2018-08-09 Klaus Schilling Formationsfähiger Kleinstsatellit und Formation aus mehreren Kleinstsatelliten
CN108910086B (zh) * 2018-06-14 2024-03-15 南京邮电大学 一种基于小卫星星团的可再入式立方星系统
CN113424074A (zh) * 2019-02-13 2021-09-21 拉姆达 4发展有限公司 基于频率切换的运行时间测量

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US3290677A (en) * 1962-12-31 1966-12-06 Trw Inc Continuous wave angle and range determining radar
JP2660017B2 (ja) * 1988-10-05 1997-10-08 一郎 中谷 宇宙構造体の相対位置・姿勢検出装置
US5092543A (en) * 1989-09-27 1992-03-03 General Electric Company Spacecraft attitude control with avoidance constraint
JPH0434310A (ja) * 1990-05-31 1992-02-05 Mitsubishi Electric Corp 宇宙機の航法装置
US5347286A (en) * 1992-02-13 1994-09-13 Trimble Navigation Limited Automatic antenna pointing system based on global positioning system (GPS) attitude information
FR2741955B1 (fr) * 1995-12-01 1998-02-06 Matra Marconi Space France Procede et dispositif de mesure d'attitude de satellite
US6072433A (en) * 1996-07-31 2000-06-06 California Institute Of Technology Autonomous formation flying sensor
JP2950279B2 (ja) * 1997-03-26 1999-09-20 日本電気株式会社 目標信号距離測定装置
US6005514A (en) * 1997-09-15 1999-12-21 United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method for attitude determination using GPS carrier phase measurements from nonaligned antennas
US5999127A (en) * 1998-10-06 1999-12-07 The Aerospace Corporation Satellite communications facilitated by synchronized nodal regressions of low earth orbits
US6150977A (en) * 1998-10-30 2000-11-21 Trw Inc. Method for enhancing the performance of a satellite communications system using multibeam antennas
US6459411B2 (en) * 1998-12-30 2002-10-01 L-3 Communications Corporation Close/intra-formation positioning collision avoidance system and method
DE19950247A1 (de) * 1999-10-18 2001-05-17 Daimler Chrysler Ag Regelungsanordnung und Regelungsverfahren für Sstelliten
US6442385B1 (en) * 1999-11-04 2002-08-27 Xm Satellite Radio, Inc. Method and apparatus for selectively operating satellites in tundra orbits to reduce receiver buffering requirements for time diversity signals
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US6289268B1 (en) * 2000-03-02 2001-09-11 Hughes Electronics Corp. Attitude determination system and method
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US7124001B2 (en) * 2003-07-11 2006-10-17 The Boeing Company Relative attitude estimator for multi-payload attitude determination

Also Published As

Publication number Publication date
JP2009536314A (ja) 2009-10-08
RU2008133983A (ru) 2010-02-27
DE602006012795D1 (de) 2010-04-22
EP1813957A1 (de) 2007-08-01
JP5007467B2 (ja) 2012-08-22
RU2419807C2 (ru) 2011-05-27
CN101375176A (zh) 2009-02-25
WO2007082929A1 (fr) 2007-07-26
EP1813957B1 (de) 2010-03-10
US8463467B2 (en) 2013-06-11
CN101375176B (zh) 2011-11-23
ES2340062T3 (es) 2010-05-28
US20110160939A1 (en) 2011-06-30

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