ES2410730R1 - Sistema compacto de generacion y control de momentos de fuerza con direccion constante - Google Patents

Sistema compacto de generacion y control de momentos de fuerza con direccion constante

Info

Publication number
ES2410730R1
ES2410730R1 ES201132118A ES201132118A ES2410730R1 ES 2410730 R1 ES2410730 R1 ES 2410730R1 ES 201132118 A ES201132118 A ES 201132118A ES 201132118 A ES201132118 A ES 201132118A ES 2410730 R1 ES2410730 R1 ES 2410730R1
Authority
ES
Spain
Prior art keywords
generation
control
compact system
force moments
constant address
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.)
Granted
Application number
ES201132118A
Other languages
English (en)
Other versions
ES2410730A2 (es
ES2410730B1 (es
Inventor
Martinez Juan Pedro Vela
Garcia Alvaro Espin
Martinez Carlos Perez
Los Santos Trigo Silvia De
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.)
Fundacion Andaluza para el Desarrollo Aeroespacial
Original Assignee
Fundacion Andaluza para el Desarrollo Aeroespacial
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 Fundacion Andaluza para el Desarrollo Aeroespacial filed Critical Fundacion Andaluza para el Desarrollo Aeroespacial
Priority to ES201132118A priority Critical patent/ES2410730B1/es
Publication of ES2410730A2 publication Critical patent/ES2410730A2/es
Publication of ES2410730R1 publication Critical patent/ES2410730R1/es
Application granted granted Critical
Publication of ES2410730B1 publication Critical patent/ES2410730B1/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01CMEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C19/00Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
    • G01C19/02Rotary gyroscopes
    • G01C19/04Details
    • G01C19/06Rotors
    • G01C19/065Means for measuring or controlling of rotors' angular velocity
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/28Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/286Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Automation & Control Theory (AREA)
  • Motorcycle And Bicycle Frame (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)

Abstract

Sistema de actuadores giroscópicos dispuestos de forma que uno de los giróscopos gira dentro de la envolvente de movimiento del otro, permitiendo una reducción sustancial del volumen necesario para conseguir un momento de fuerza determinado con una dirección constante.
ES201132118A 2011-12-28 2011-12-28 Sistema compacto de generacion y control de momentos de fuerza con direccion constante Active ES2410730B1 (es)

Priority Applications (1)

Application Number Priority Date Filing Date Title
ES201132118A ES2410730B1 (es) 2011-12-28 2011-12-28 Sistema compacto de generacion y control de momentos de fuerza con direccion constante

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES201132118A ES2410730B1 (es) 2011-12-28 2011-12-28 Sistema compacto de generacion y control de momentos de fuerza con direccion constante

Publications (3)

Publication Number Publication Date
ES2410730A2 ES2410730A2 (es) 2013-07-02
ES2410730R1 true ES2410730R1 (es) 2013-10-07
ES2410730B1 ES2410730B1 (es) 2014-08-12

Family

ID=48614232

Family Applications (1)

Application Number Title Priority Date Filing Date
ES201132118A Active ES2410730B1 (es) 2011-12-28 2011-12-28 Sistema compacto de generacion y control de momentos de fuerza con direccion constante

Country Status (1)

Country Link
ES (1) ES2410730B1 (es)

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005095891A1 (en) * 2004-04-02 2005-10-13 Eco Bond Trading Pte Ltd Gyroscope apparatus
EP1993017A1 (fr) * 2006-02-28 2008-11-19 Advanced Dynamic Systems, S.L. Actionneur gyroscopique permettant de commander des satellites
US20110011982A1 (en) * 2009-07-20 2011-01-20 Jason Herman Modular control moment gyroscope (cmg) system for spacecraft attitude control

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2005095891A1 (en) * 2004-04-02 2005-10-13 Eco Bond Trading Pte Ltd Gyroscope apparatus
EP1993017A1 (fr) * 2006-02-28 2008-11-19 Advanced Dynamic Systems, S.L. Actionneur gyroscopique permettant de commander des satellites
US20110011982A1 (en) * 2009-07-20 2011-01-20 Jason Herman Modular control moment gyroscope (cmg) system for spacecraft attitude control

Also Published As

Publication number Publication date
ES2410730A2 (es) 2013-07-02
ES2410730B1 (es) 2014-08-12

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