FR3110552B1 - Orbiting vehicle with a rollable and deployable membrane for attitude and orbit control - Google Patents

Orbiting vehicle with a rollable and deployable membrane for attitude and orbit control

Info

Publication number
FR3110552B1
FR3110552B1 FR2005135A FR2005135A FR3110552B1 FR 3110552 B1 FR3110552 B1 FR 3110552B1 FR 2005135 A FR2005135 A FR 2005135A FR 2005135 A FR2005135 A FR 2005135A FR 3110552 B1 FR3110552 B1 FR 3110552B1
Authority
FR
France
Prior art keywords
attitude
vehicle
membrane
instantaneous
rollable
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
FR2005135A
Other languages
French (fr)
Other versions
FR3110552A1 (en
Inventor
Anne Giovannini
Stéphane Vezain
Alexandre Garus
Gonzalez Jose-Alvaro Perez
Bertrand Raffier
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.)
Centre National d'Études Spatiales
Thales SA
Original Assignee
Centre National d'Études Spatiales
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 Centre National d'Études Spatiales, Thales SA filed Critical Centre National d'Études Spatiales
Priority to FR2005135A priority Critical patent/FR3110552B1/en
Publication of FR3110552A1 publication Critical patent/FR3110552A1/en
Application granted granted Critical
Publication of FR3110552B1 publication Critical patent/FR3110552B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B64G1/2221—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the manner of deployment
    • B64G1/2225—Rolling or unfurling
    • 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
    • B64G1/407—Solar sailing
    • 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
    • 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
    • B64G1/222—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state
    • B64G1/2229—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles for deploying structures between a stowed and deployed state characterised by the deployment actuating mechanism
    • 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
    • B64G1/62—Systems for re-entry into the earth's atmosphere; Retarding or landing devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Motorcycle And Bicycle Frame (AREA)

Abstract

L’invention concerne un véhicule (100) en orbite ayant une position instantanée et une attitude instantanée, ledit véhicule (100) étant destiné à prendre une position de consigne et une attitude de consigne sur son orbite, comprenant: une caisse (101) ; N rouleaux de stockage (R1, R2) reliés à la caisse (101), N étant un entier supérieur ou égal à 1, chacun des N rouleaux de stockage (R1, R2) supportant une membrane (M1, M2), ladite membrane étant apte à passer d’une configuration enroulée autour d’un premier axe principal (X1, X2) à une configuration déployée selon un premier axe secondaire (Y1, Y2) sensiblement perpendiculaire au premier axe principal (X1, X2), et vice versa ; un ensemble de capteurs (103) de la position instantanée et l’attitude instantanée du véhicule (100); un dispositif d’actionnement (104) d’au moins un parmi les N rouleaux de stockage (R1, R2) entre la configuration enroulée et la configuration déployée de la membrane (M1, M2) pour placer le véhicule (100) à une nouvelle position instantanée et une nouvelle attitude instantanée; un asservissement (105) du dispositif d’actionnement (104) selon la nouvelle position instantanée et la nouvelle attitude instantanée par rapport à la position de consigne et l’attitude de consigne. Figure pour l’abrégé : Fig. 4The invention relates to an orbiting vehicle (100) having an instantaneous position and an instantaneous attitude, said vehicle (100) being intended to take a set position and a set attitude on its orbit, comprising: a casing (101); N storage rollers (R1, R2) connected to the casing (101), N being an integer greater than or equal to 1, each of the N storage rollers (R1, R2) supporting a membrane (M1, M2), said membrane being capable of going from a configuration wound around a first principal axis (X1, X2) to a configuration deployed along a first secondary axis (Y1, Y2) substantially perpendicular to the first principal axis (X1, X2), and vice versa; a set of sensors (103) of the instantaneous position and the instantaneous attitude of the vehicle (100); an actuation device (104) for at least one of the N storage rollers (R1, R2) between the wound and unwound configurations of the membrane (M1, M2) to place the vehicle (100) at a new instantaneous position and attitude; a control system (105) for the actuation device (104) according to the new instantaneous position and attitude relative to the setpoint position and attitude. Figure for the abstract: Fig. 4

FR2005135A 2020-05-20 2020-05-20 Orbiting vehicle with a rollable and deployable membrane for attitude and orbit control Active FR3110552B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR2005135A FR3110552B1 (en) 2020-05-20 2020-05-20 Orbiting vehicle with a rollable and deployable membrane for attitude and orbit control

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2005135 2020-05-20
FR2005135A FR3110552B1 (en) 2020-05-20 2020-05-20 Orbiting vehicle with a rollable and deployable membrane for attitude and orbit control

Publications (2)

Publication Number Publication Date
FR3110552A1 FR3110552A1 (en) 2021-11-26
FR3110552B1 true FR3110552B1 (en) 2026-07-24

Family

ID=73013492

Family Applications (1)

Application Number Title Priority Date Filing Date
FR2005135A Active FR3110552B1 (en) 2020-05-20 2020-05-20 Orbiting vehicle with a rollable and deployable membrane for attitude and orbit control

Country Status (1)

Country Link
FR (1) FR3110552B1 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2025239432A1 (en) * 2024-05-17 2025-11-20 株式会社Bull Spacecraft and method for manufacturing same

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2897843B1 (en) * 2006-02-27 2009-03-06 Eads Space Transp Sas Soc Par SATELLITE AEROPREINAGE SAIL
DE102011107208A1 (en) * 2011-07-13 2013-01-17 Frank Ellinghaus Mobile solar glider space powerhouse and coupled solar glider power plants for space-based energy generation and generation
FR2998876B1 (en) * 2012-12-05 2015-07-17 Thales Sa DEVICE FOR DEPLOYING AND REPLOYING A FLEXIBLE STRUCTURE, FLEXIBLE DEPLOYABLE STRUCTURE AND SATELLITE PROVIDED WITH SUCH A DEVICE
FR3024228B1 (en) * 2014-07-25 2018-02-09 Thales DEPLOYABLE STRUCTURE WITH METER-RIBBON
FR3028842A1 (en) * 2014-11-21 2016-05-27 Thales Sa RETRACTABLE DEPLOYABLE STRUCTURE WITH METER-RIBBON
FR3044639B1 (en) * 2015-12-02 2018-01-05 Thales DEPLOYABLE STRUCTURE COMPRISING A SET OF SOLAR GENERATORS, SYSTEM FOR DEPLOYING SUCH A DEPLOYABLE STRUCTURE AND SATELLITE COMPRISING SUCH A SYSTEM
US11338942B2 (en) * 2016-06-14 2022-05-24 Richard Stuart Blomquist Spacecraft and control method

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FR3110552A1 (en) 2021-11-26

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