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FR3089623B1 - Procédé et système de mesure de l’attitude d’un appendice relie a une plateforme d’un satellite - Google Patents

Procédé et système de mesure de l’attitude d’un appendice relie a une plateforme d’un satellite Download PDF

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Publication number
FR3089623B1
FR3089623B1 FR1872656A FR1872656A FR3089623B1 FR 3089623 B1 FR3089623 B1 FR 3089623B1 FR 1872656 A FR1872656 A FR 1872656A FR 1872656 A FR1872656 A FR 1872656A FR 3089623 B1 FR3089623 B1 FR 3089623B1
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FR
France
Prior art keywords
attitude
appendix
platform
appendage
measuring
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.)
Active
Application number
FR1872656A
Other languages
English (en)
Other versions
FR3089623A1 (fr
Inventor
Brice Dellandrea
Sébastien Dazin
Etienne Brouillard
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.)
Thales SA
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
Priority to FR1872656A priority Critical patent/FR3089623B1/fr
Publication of FR3089623A1 publication Critical patent/FR3089623A1/fr
Application granted granted Critical
Publication of FR3089623B1 publication Critical patent/FR3089623B1/fr
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/02—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 by astronomical means
    • 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
    • B64G1/244—Spacecraft control 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
    • B64G1/24—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
    • B64G1/361—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using star sensors
    • 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
    • B64G1/66—Arrangements or adaptations of apparatus or instruments, not otherwise provided for
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G4/00—Tools specially adapted for use in space
    • B64G2004/005—Robotic manipulator systems for use in space

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Navigation (AREA)

Abstract

L’invention se rapporte à un procédé de mesure de l’attitude d’un appendice (AP) d’un satellite (SAT), le satellite (SAT) comprenant un senseur stellaire de plateforme (SP), monté sur une plateforme (PF) du satellite (SAT), un système de traitement de données (CC, CL), et un senseur stellaire d’appendice (SA), relié au système de traitement de données (CC, CL), monté sur l’appendice (AP), le procédé de mesure comprenant les étapes suivantes : a) acquisition, par le senseur stellaire de plateforme (SP), d’images de l’environnement extérieur de la plateforme (PF) ; b) détermination, par le système de traitement de données (CC, CL), de l’attitude de la plateforme (PF) à partir desdites images ; c) acquisition, par le senseur stellaire d’appendice (SA), d’images de l’environnement extérieur de l’appendice (AP) ; d) détermination, par le système de traitement de données (CC, CL), de l’attitude de l’appendice (AP), à partir des images de l’environnement extérieur de l’appendice (AP) acquises par le senseur stellaire d’appendice (SA), et d’une estimation de l’attitude de l’appendice (AP) par rapport à l’attitude de la plateforme (PF). Figure pour l’abrégé : Fig. 1
FR1872656A 2018-12-11 2018-12-11 Procédé et système de mesure de l’attitude d’un appendice relie a une plateforme d’un satellite Active FR3089623B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1872656A FR3089623B1 (fr) 2018-12-11 2018-12-11 Procédé et système de mesure de l’attitude d’un appendice relie a une plateforme d’un satellite

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1872656A FR3089623B1 (fr) 2018-12-11 2018-12-11 Procédé et système de mesure de l’attitude d’un appendice relie a une plateforme d’un satellite

Publications (2)

Publication Number Publication Date
FR3089623A1 FR3089623A1 (fr) 2020-06-12
FR3089623B1 true FR3089623B1 (fr) 2021-10-08

Family

ID=67185096

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1872656A Active FR3089623B1 (fr) 2018-12-11 2018-12-11 Procédé et système de mesure de l’attitude d’un appendice relie a une plateforme d’un satellite

Country Status (1)

Country Link
FR (1) FR3089623B1 (fr)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN115649482B (zh) * 2022-10-27 2024-11-08 长光卫星技术股份有限公司 一种星敏感器高稳定性热控装置及方法

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2110865C (fr) * 1992-12-08 1998-07-14 Naoshi Suzuki Correction des effets dus au courant d'obscurite dans les pixels d'etoiles
US5412574A (en) * 1993-05-14 1995-05-02 Hughes Aircraft Company Method of attitude determination using earth and star sensors
US5978716A (en) * 1997-05-28 1999-11-02 Space Systems/Loral, Inc. Satellite imaging control system for non-repeatable error
US6978966B2 (en) * 2004-02-02 2005-12-27 The Boeing Company Reflector deployment error estimation
DE102013108711B4 (de) * 2013-08-12 2016-07-14 Jena-Optronik Gmbh Verfahren zum Betrieb eines Lage- und Orbit-Steuersystems und Lage- und Orbit-Steuersystem
WO2018085683A1 (fr) * 2016-11-03 2018-05-11 The Charles Stark Draper Laboratory, Inc. Réseau d'imagerie photonique

Also Published As

Publication number Publication date
FR3089623A1 (fr) 2020-06-12

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