BR112016024524A2 - ?processo para implantar uma constelação de satélites? - Google Patents

?processo para implantar uma constelação de satélites?

Info

Publication number
BR112016024524A2
BR112016024524A2 BR112016024524A BR112016024524A BR112016024524A2 BR 112016024524 A2 BR112016024524 A2 BR 112016024524A2 BR 112016024524 A BR112016024524 A BR 112016024524A BR 112016024524 A BR112016024524 A BR 112016024524A BR 112016024524 A2 BR112016024524 A2 BR 112016024524A2
Authority
BR
Brazil
Prior art keywords
satellites
deploying
altitude
satellite constellation
guiding
Prior art date
Application number
BR112016024524A
Other languages
English (en)
Other versions
BR112016024524B1 (pt
Inventor
Marchandise Frédéric
Simontacchi Pamela
Mathieu Perrine
Original Assignee
Safran Aircraft Engines
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 Safran Aircraft Engines filed Critical Safran Aircraft Engines
Publication of BR112016024524A2 publication Critical patent/BR112016024524A2/pt
Publication of BR112016024524B1 publication Critical patent/BR112016024524B1/pt

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
    • B64G1/2427—Transfer orbits
    • 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

Abstract

a invenção refere-se a um processo para implantar uma constelação de satélite, que compreende: implantar, por meio de um único lançador, uma pluralidade de satélites (10) em uma altitude inicial acima de uma órbita inicial; guiar os ditos satélites (20) de maneira que cada satélite atinja uma altitude de desvio entre um conjunto de desvio, em que as órbitas dos satélites diferentes sejam deslocadas (30) em relação uma a outra pelo potencial gravitacional da terra; guiar os satélites de maneira que eles sejam movidos (40) sequencialmente a fim de atingir a mesma altitude final, o dito movimento sequencial sendo realizado de maneira que os satélites descrevam órbitas finais que são angularmente deslocadas em relação uma a outra.
BR112016024524-5A 2014-04-24 2015-04-21 Processo para implantar uma constelação de satélites BR112016024524B1 (pt)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
FR1453690A FR3020348B1 (fr) 2014-04-24 2014-04-24 Procede de deploiement d'une constellation de satellites
FR1453690 2014-04-24
PCT/FR2015/051074 WO2015162370A1 (fr) 2014-04-24 2015-04-21 Procédé de déploiement d'une constellation de satellites

Publications (2)

Publication Number Publication Date
BR112016024524A2 true BR112016024524A2 (pt) 2017-08-15
BR112016024524B1 BR112016024524B1 (pt) 2022-05-10

Family

ID=52630398

Family Applications (1)

Application Number Title Priority Date Filing Date
BR112016024524-5A BR112016024524B1 (pt) 2014-04-24 2015-04-21 Processo para implantar uma constelação de satélites

Country Status (10)

Country Link
US (1) US11066190B2 (pt)
EP (1) EP3134322B1 (pt)
JP (1) JP6659576B2 (pt)
CN (1) CN106458337B (pt)
BR (1) BR112016024524B1 (pt)
CA (1) CA2946233C (pt)
FR (1) FR3020348B1 (pt)
IL (1) IL248390B2 (pt)
RU (2) RU2021133706A (pt)
WO (1) WO2015162370A1 (pt)

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CN107329146B (zh) * 2017-07-05 2021-06-15 中国人民解放军战略支援部队航天工程大学 一种导航卫星低轨监测星座的优化设计方法
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WO2020240824A1 (ja) * 2019-05-31 2020-12-03 三菱電機株式会社 衛星コンステレーション形成システム、衛星コンステレーション形成方法、衛星コンステレーション、および地上装置
JP7068764B2 (ja) * 2019-05-31 2022-05-17 三菱電機株式会社 衛星コンステレーション形成システム、衛星コンステレーション形成方法、衛星コンステレーション、デオービット方法、デブリ回収方法、および地上装置
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CN112785680B (zh) * 2019-11-07 2023-01-24 上海莉莉丝科技股份有限公司 描述三维虚拟空间中物体关系的方法、系统、设备和介质
CN111591469B (zh) * 2020-03-03 2021-12-07 航天科工空间工程发展有限公司 一种低轨星座系统相位保持方法、系统、设备和存储介质
WO2022270337A1 (ja) * 2021-06-23 2022-12-29 三菱電機株式会社 衛星コンステレーション維持方法、衛星コンステレーション、ロケット打上げ方法、地上設備、コマンド送信方法、および、コマンド送信プログラム
CN114006646B (zh) * 2021-09-27 2023-09-29 中国人民解放军战略支援部队航天工程大学 一种Walker星座构型维持的轨道控制频次分析方法及装置

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Also Published As

Publication number Publication date
RU2016145879A3 (pt) 2018-10-31
CA2946233C (fr) 2022-08-23
US11066190B2 (en) 2021-07-20
EP3134322A1 (fr) 2017-03-01
BR112016024524B1 (pt) 2022-05-10
CA2946233A1 (fr) 2015-10-29
EP3134322B1 (fr) 2019-11-20
CN106458337B (zh) 2019-09-20
FR3020348A1 (fr) 2015-10-30
IL248390B2 (en) 2023-02-01
CN106458337A (zh) 2017-02-22
JP6659576B2 (ja) 2020-03-04
WO2015162370A1 (fr) 2015-10-29
FR3020348B1 (fr) 2016-05-13
RU2016145879A (ru) 2018-05-24
IL248390B (en) 2022-10-01
US20170043885A1 (en) 2017-02-16
JP2017513765A (ja) 2017-06-01
IL248390A0 (en) 2016-11-30
RU2021133706A (ru) 2021-11-26

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B06U Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette]
B350 Update of information on the portal [chapter 15.35 patent gazette]
B09A Decision: intention to grant [chapter 9.1 patent gazette]
B16A Patent or certificate of addition of invention granted [chapter 16.1 patent gazette]

Free format text: PRAZO DE VALIDADE: 20 (VINTE) ANOS CONTADOS A PARTIR DE 12/04/2015, OBSERVADAS AS CONDICOES LEGAIS