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 constanteInfo
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
- G01C19/00—Gyroscopes; Turn-sensitive devices using vibrating masses; Turn-sensitive devices without moving masses; Measuring angular rate using gyroscopic effects
- G01C19/02—Rotary gyroscopes
- G01C19/04—Details
- G01C19/06—Rotors
- G01C19/065—Means for measuring or controlling of rotors' angular velocity
-
- 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
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/286—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using control momentum gyroscopes (CMGs)
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/08—Control 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.
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)
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 |
-
2011
- 2011-12-28 ES ES201132118A patent/ES2410730B1/es active Active
Patent Citations (3)
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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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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