DE602004021042D1 - Satellitensystem in ultrahoher höhe mit sonnensynchroner umlaufbahn - Google Patents

Satellitensystem in ultrahoher höhe mit sonnensynchroner umlaufbahn

Info

Publication number
DE602004021042D1
DE602004021042D1 DE602004021042T DE602004021042T DE602004021042D1 DE 602004021042 D1 DE602004021042 D1 DE 602004021042D1 DE 602004021042 T DE602004021042 T DE 602004021042T DE 602004021042 T DE602004021042 T DE 602004021042T DE 602004021042 D1 DE602004021042 D1 DE 602004021042D1
Authority
DE
Germany
Prior art keywords
ultra
satellite system
sun synchronous
synchronous carriage
high satellite
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
DE602004021042T
Other languages
English (en)
Inventor
Junichiro Kawaguchi
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.)
Japan Aerospace Exploration Agency JAXA
Original Assignee
Japan Aerospace Exploration Agency JAXA
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 Japan Aerospace Exploration Agency JAXA filed Critical Japan Aerospace Exploration Agency JAXA
Publication of DE602004021042D1 publication Critical patent/DE602004021042D1/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
    • B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1007—Communications satellites
    • 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
    • B64G1/1021—Earth observation satellites
    • 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
    • B64G1/2423—Sun-synchronous orbits

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Radio Relay Systems (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
DE602004021042T 2004-06-22 2004-06-22 Satellitensystem in ultrahoher höhe mit sonnensynchroner umlaufbahn Expired - Lifetime DE602004021042D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
PCT/JP2004/008742 WO2005123507A1 (ja) 2004-06-22 2004-06-22 超高々度太陽同期軌道衛星システム

Publications (1)

Publication Number Publication Date
DE602004021042D1 true DE602004021042D1 (de) 2009-06-18

Family

ID=35509555

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004021042T Expired - Lifetime DE602004021042D1 (de) 2004-06-22 2004-06-22 Satellitensystem in ultrahoher höhe mit sonnensynchroner umlaufbahn

Country Status (5)

Country Link
US (1) US7806369B2 (de)
EP (1) EP1783050B1 (de)
JP (1) JP4465455B2 (de)
DE (1) DE602004021042D1 (de)
WO (1) WO2005123507A1 (de)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10342866A1 (de) * 2003-09-15 2005-04-21 Eads Astrium Gmbh Verfahren zur Lagebestimmung eines Raumfahrzeuges mit Hilfe eines Richtungsvektors und einer Gesamtdrallmessung
US8437892B1 (en) * 2010-01-20 2013-05-07 The United States Of America, As Represented By The Secretary Of The Navy Method and system for establishment and maintenance of a global formation of directionally-fixed spacecraft without the use of expendable mass
US8511614B2 (en) * 2010-03-22 2013-08-20 Raytheon Company Satellite system providing optimal space situational awareness
KR20120071238A (ko) * 2010-12-22 2012-07-02 한국전자통신연구원 지구 동기 위성을 이용한 범 지구 위성 항법 시스템
US9182584B2 (en) 2012-07-31 2015-11-10 Honeywell International Inc. Method and system for evaluating stare-time by a pointing system
US9487309B2 (en) * 2013-05-20 2016-11-08 Kratos Integral Holdings, Llc Eccentricity control for geosynchronous satellites
CN106021726B (zh) * 2016-05-19 2019-02-15 北京航空航天大学 一种发射观测卫星到冻结轨道的偏心率控制方法
CN106564622B (zh) * 2016-11-02 2019-04-09 北京控制工程研究所 一种基于视线测量的同步轨道卫星相对倾角远距离修正方法
WO2020217340A1 (ja) * 2019-04-24 2020-10-29 三菱電機株式会社 衛星コンステレーション、地上設備および人工衛星
WO2022029864A1 (ja) 2020-08-04 2022-02-10 三菱電機株式会社 信号処理装置、信号処理方法、受信器及び光通信システム
CN113654512A (zh) * 2021-08-13 2021-11-16 中国电子科技集团公司第十四研究所 一种空间目标光学可见性分析方法
CN114491694B (zh) * 2022-01-17 2024-06-25 北京航空航天大学 一种基于虚幻引擎的空间目标数据集构建方法
US11930583B1 (en) 2022-09-08 2024-03-12 Ali Kaddoura Heat conditioning through deflection/reflection/absorption of electromagnetic waves
CN115540877B (zh) * 2022-09-14 2023-08-25 哈尔滨工业大学 一种考虑地球扁率的太阳光照系数确定方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5183225A (en) * 1989-01-09 1993-02-02 Forward Robert L Statite: spacecraft that utilizes sight pressure and method of use
JPH10258799A (ja) 1997-03-18 1998-09-29 Fujitsu Ltd 太陽同期軌道衛星システム
AU1326901A (en) * 1999-08-16 2001-03-13 Mobile Communications Holdings, Inc. Constellation of elliptical orbit satellites with line of apsides lying in or near the equatorial plane
JP2002037200A (ja) 2000-07-28 2002-02-06 Mitsubishi Electric Corp 軌道傾斜角を有する衛星
JP3613188B2 (ja) 2001-03-01 2005-01-26 三菱電機株式会社 高高度傾斜軌道衛星通信測位システム
JP4472240B2 (ja) * 2002-08-28 2010-06-02 Ｎｅｃ東芝スペースシステム株式会社 通信衛星システム

Also Published As

Publication number Publication date
US7806369B2 (en) 2010-10-05
WO2005123507A1 (ja) 2005-12-29
EP1783050A1 (de) 2007-05-09
US20080029650A1 (en) 2008-02-07
JP4465455B2 (ja) 2010-05-19
EP1783050B1 (de) 2009-05-06
EP1783050A4 (de) 2007-09-12
JPWO2005123507A1 (ja) 2008-04-10

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