ES3068826T3 - Device for controlling the angular velocity of a spacecraft, and corresponding spacecraft - Google Patents

Device for controlling the angular velocity of a spacecraft, and corresponding spacecraft

Info

Publication number
ES3068826T3
ES3068826T3 ES23837694T ES23837694T ES3068826T3 ES 3068826 T3 ES3068826 T3 ES 3068826T3 ES 23837694 T ES23837694 T ES 23837694T ES 23837694 T ES23837694 T ES 23837694T ES 3068826 T3 ES3068826 T3 ES 3068826T3
Authority
ES
Spain
Prior art keywords
stator
spacecraft
rotor
respect
controlling
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
ES23837694T
Other languages
English (en)
Inventor
Baptiste Brault
Kristen Lagadec
Maxime Senes
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
Airbus Defence and Space SAS
Original Assignee
Centre National d'Études Spatiales
Airbus Defence and Space SAS
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, Airbus Defence and Space SAS filed Critical Centre National d'Études Spatiales
Application granted granted Critical
Publication of ES3068826T3 publication Critical patent/ES3068826T3/es
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
    • B64G1/24—Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
    • 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
    • B64G1/245—Attitude control algorithms for spacecraft attitude control
    • 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
    • B64G3/00—Observing or tracking cosmonautic vehicles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G7/00—Simulating cosmonautic conditions, e.g. for conditioning crews
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M99/00—Subject matter not provided for in other groups of this subclass
    • G01M99/008—Subject matter not provided for in other groups of this subclass by doing functionality tests

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • General Physics & Mathematics (AREA)
  • Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Automation & Control Theory (AREA)
  • Astronomy & Astrophysics (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Environmental & Geological Engineering (AREA)
  • General Life Sciences & Earth Sciences (AREA)
  • Geochemistry & Mineralogy (AREA)
  • Geology (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Magnetic Bearings And Hydrostatic Bearings (AREA)
  • Dynamo-Electric Clutches, Dynamo-Electric Brakes (AREA)

Abstract

La invención se refiere a un dispositivo (1) para controlar la velocidad angular de una nave espacial fuera de servicio, que comprende: - un estator (3) y un rotor (4) móviles alrededor de un eje (A21) de rotación con respecto al estator, el estator (3) comprende un cuerpo (6) conductor de electricidad y no ferromagnético, mientras que el rotor (4) comprende un sistema magnetizado (7) configurado para inducir, en el estator (3), corrientes parásitas para frenar el movimiento relativo del rotor (4) con respecto al estator (3); - un imán de suspensión magnética (11) destinado a cooperar con un campo magnético generado por una fuente externa para suspender magnéticamente el rotor (4) con respecto al estator (3). El dispositivo (1) consta de uno o más materiales no ferromagnéticos en una zona (11ZI) de influencia del campo magnético generado por el imán de suspensión magnética. (Traducción automática con Google Translate, sin valor legal)
ES23837694T 2023-03-13 2023-12-22 Device for controlling the angular velocity of a spacecraft, and corresponding spacecraft Active ES3068826T3 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR2302125A FR3146660B1 (fr) 2023-03-13 2023-03-13 Dispositif de contrôle de vitesse angulaire d'un engin spatial et engin spatial correspondant.
PCT/EP2023/087596 WO2024188504A1 (fr) 2023-03-13 2023-12-22 Dispositif de contrôle de vitesse angulaire d'un engin spatial et engin spatial correspondant

Publications (1)

Publication Number Publication Date
ES3068826T3 true ES3068826T3 (en) 2026-06-02

Family

ID=87571409

Family Applications (1)

Application Number Title Priority Date Filing Date
ES23837694T Active ES3068826T3 (en) 2023-03-13 2023-12-22 Device for controlling the angular velocity of a spacecraft, and corresponding spacecraft

Country Status (5)

Country Link
US (1) US20260008566A1 (es)
EP (1) EP4680530B1 (es)
ES (1) ES3068826T3 (es)
FR (1) FR3146660B1 (es)
WO (1) WO2024188504A1 (es)

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
BE858877A (fr) * 1977-09-20 1978-01-16 Organisation Europ De Rech S S Roue d'inertie a suspension magnetique
EP2671804B1 (en) 2012-06-07 2014-04-30 Astrium Limited Space object capture
US9663250B1 (en) * 2012-09-28 2017-05-30 Ball Aerospace & Technologies Corp. Method and apparatus for passively slowing the spin rate of orbital objects
FR2999537B1 (fr) 2012-12-19 2015-02-20 Astrium Sas Systeme et procede de capture et d'elimination d'un debris spatial
FR3026858B1 (fr) * 2014-10-02 2016-12-09 Airbus Defence & Space Sas Procede de controle d'attitude d'un satellite en mode survie, satellite adapte et procede de commande a distance d'un tel satellite
FR3058393A1 (fr) 2016-11-10 2018-05-11 Airbus Defence And Space Sas Engin spatial comprenant des moyens de controle actif d’attitude et des moyens de controle passif d’attitude
CN106406329B (zh) * 2016-11-21 2019-06-11 哈尔滨工业大学 一种基于永磁涡流效应的空间翻滚目标消旋控制方法
CN111439400B (zh) * 2020-04-15 2024-10-22 中国人民解放军国防科技大学 一种模拟空间目标电磁-涡流消旋的地面试验系统
FR3127481B1 (fr) * 2021-09-24 2023-10-20 Airbus Defence & Space Sas Dispositif de contrôle de vitesse angulaire d’un engin spatial et engin spatial correspondant.

Also Published As

Publication number Publication date
EP4680530C0 (fr) 2026-02-25
EP4680530B1 (fr) 2026-02-25
US20260008566A1 (en) 2026-01-08
FR3146660A1 (fr) 2024-09-20
WO2024188504A1 (fr) 2024-09-19
EP4680530A1 (fr) 2026-01-21
FR3146660B1 (fr) 2026-02-20