BR112016014819A2 - Conjunto de giroscópio de momento de controle que inclui vários giroscópios de momento de controle, unidade de controle de atitude, sistema de controle de atitude e plataforma espacial - Google Patents
Conjunto de giroscópio de momento de controle que inclui vários giroscópios de momento de controle, unidade de controle de atitude, sistema de controle de atitude e plataforma espacialInfo
- Publication number
- BR112016014819A2 BR112016014819A2 BR112016014819A BR112016014819A BR112016014819A2 BR 112016014819 A2 BR112016014819 A2 BR 112016014819A2 BR 112016014819 A BR112016014819 A BR 112016014819A BR 112016014819 A BR112016014819 A BR 112016014819A BR 112016014819 A2 BR112016014819 A2 BR 112016014819A2
- Authority
- BR
- Brazil
- Prior art keywords
- control
- attitude control
- attitude
- moment
- gyroscopes
- Prior art date
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)
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/10—Artificial satellites; Systems of such satellites; Interplanetary vehicles
-
- 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
- F16M2200/00—Details of stands or supports
- F16M2200/06—Arms
- F16M2200/065—Arms with a special structure, e.g. reinforced or adapted for space reduction
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Astronomy & Astrophysics (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Abstract
CONJUNTO DE GIROSCÓPIO DE MOMENTO DE CONTROLE QUE INCLUI VÁRIOS GIROSCÓPIOS DE MOMENTO DE CONTROLE, UNIDADE DE CONTROLE DE ATITUDE, SISTEMA DE CONTROLE DE ATITUDE E PLATAFORMA ESPACIAL. A presente invenção refere-se, de forma geral, ao controle de atitude e, em particular, ao controle da atitude de uma plataforma espacial, convenientemente de um satélite e/ou de uma espaçonave. Detalhadamente, um aspecto da presente invenção refere-se ao uso, em um sistema de controle de atitude (100), de vários Giroscópios de Momento de Controle (3, 41, 42, 43, 44, 61, 62, 63, 64) com revoluções cardan limitadas. Além disso, outro aspecto da presente invenção refere-se a uma lógica aprimorada de controle de um conjunto de Giroscópio de Momento de Controle (4, 6, 120) de um sistema de controle de atitude (100).
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
IT001067A ITTO20131067A1 (it) | 2013-12-23 | 2013-12-23 | Sistema di controllo di assetto per applicazioni satellitari agili |
PCT/IB2014/067282 WO2015097672A2 (en) | 2013-12-23 | 2014-12-23 | Attitude control for agile satellite applications |
Publications (1)
Publication Number | Publication Date |
---|---|
BR112016014819A2 true BR112016014819A2 (pt) | 2017-08-08 |
Family
ID=50116102
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
BR112016014819A BR112016014819A2 (pt) | 2013-12-23 | 2014-12-23 | Conjunto de giroscópio de momento de controle que inclui vários giroscópios de momento de controle, unidade de controle de atitude, sistema de controle de atitude e plataforma espacial |
Country Status (13)
Country | Link |
---|---|
US (2) | US10703511B2 (pt) |
EP (2) | EP3216705B1 (pt) |
KR (1) | KR102266872B1 (pt) |
CN (2) | CN106068440B (pt) |
AU (2) | AU2014372139B2 (pt) |
BR (1) | BR112016014819A2 (pt) |
EA (2) | EA201691308A1 (pt) |
ES (1) | ES2694691T3 (pt) |
IT (1) | ITTO20131067A1 (pt) |
MX (1) | MX2016008286A (pt) |
PL (1) | PL3087006T3 (pt) |
SG (2) | SG11201604913TA (pt) |
WO (1) | WO2015097672A2 (pt) |
Families Citing this family (12)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
ITTO20131067A1 (it) * | 2013-12-23 | 2015-06-24 | Thales Alenia Space Italia S P A C On Unico Socio | Sistema di controllo di assetto per applicazioni satellitari agili |
US11221633B2 (en) * | 2016-05-17 | 2022-01-11 | Raytheon Company | Gyroscopic attitude control system |
CN107089348B (zh) * | 2017-04-01 | 2019-04-30 | 中国空间技术研究院 | 基于多柔性附件卫星动力学优化控制模式的在轨故障对策方法 |
US10276997B1 (en) | 2017-10-06 | 2019-04-30 | Honeywell International Inc. | Wire assembly including clockspring passes |
CN109828595A (zh) * | 2019-01-31 | 2019-05-31 | 中国人民解放军国防科技大学 | 一种失效空间航天器终端接近可行性分析方法 |
CN110329548B (zh) * | 2019-05-24 | 2023-01-17 | 中国人民解放军63789部队 | 航天器在轨转偏置控制下飞轮系统重构方法 |
CN110658838B (zh) * | 2019-09-19 | 2022-10-28 | 北京控制工程研究所 | 一种敏捷航天器三轴机动角速度实时计算方法及系统 |
CN110658837B (zh) * | 2019-09-19 | 2020-10-23 | 北京控制工程研究所 | 一种控制力矩陀螺故障情况下的平稳重构方法 |
CN111897355B (zh) * | 2020-08-06 | 2022-09-13 | 中国科学院微小卫星创新研究院 | 一种卫星姿态机动轨迹规划方法 |
CN112061425B (zh) * | 2020-09-08 | 2022-04-08 | 上海航天控制技术研究所 | 一种敏捷小卫星星敏感器受地气光干扰的规避方法 |
CN114313311B (zh) * | 2022-03-04 | 2022-05-27 | 中国人民解放军战略支援部队航天工程大学 | 一种多体变构卫星的拓扑构型 |
CN117330049B (zh) * | 2023-11-27 | 2024-01-30 | 中北大学 | 基于奇异面的腔内反射高鲁棒性角速度传感器及测量方法 |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US1380336A (en) * | 1920-11-26 | 1921-05-31 | Gyroscopic device and method | |
US3251955A (en) * | 1963-09-03 | 1966-05-17 | Honeywell Inc | Current transmitting arrangement for instruments |
US6154691A (en) * | 1997-09-02 | 2000-11-28 | Honeywell International Inc. | Orienting a satellite with controlled momentum gyros |
US6135392A (en) * | 1998-09-29 | 2000-10-24 | Hughes Electronics Corporation | Spacecraft attitude control actuator and method |
FR2826470B1 (fr) * | 2001-06-26 | 2003-09-19 | Astrium Sas | Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes |
US6772978B2 (en) * | 2002-02-22 | 2004-08-10 | Honeywell International Inc. | Dynamic unbalance compensation system and method |
FR2837580B1 (fr) * | 2002-03-21 | 2005-06-03 | Astrium Sas | Actionneur gyroscopique de pilotage de l'attitude d'un vehicule spatial |
US6681649B2 (en) | 2002-04-03 | 2004-01-27 | Honeywell International Inc. | Inertial control and measurement system |
US7014150B2 (en) * | 2004-07-30 | 2006-03-21 | Honeywell International Inc. | Method and system for optimizing torque in a CMG array |
US7805226B2 (en) * | 2006-09-29 | 2010-09-28 | Honeywell International Inc. | Hierarchical strategy for singularity avoidance in arrays of control moment gyroscopes |
US8020809B2 (en) * | 2007-04-18 | 2011-09-20 | Ithaco Space Systems, Inc. | Direct torque actuator control for control moment gyroscope |
US7997157B2 (en) * | 2008-02-11 | 2011-08-16 | Honeywell International Inc. | Control moment gyroscope |
CN100565405C (zh) * | 2008-09-12 | 2009-12-02 | 航天东方红卫星有限公司 | 一种操纵律奇异回避的航天器姿态控制系统 |
WO2010135421A2 (en) * | 2009-05-19 | 2010-11-25 | University Of Florida Research Foundation, Inc. | Attitude control system for small satellites |
US20110011982A1 (en) * | 2009-07-20 | 2011-01-20 | Jason Herman | Modular control moment gyroscope (cmg) system for spacecraft attitude control |
CN101891018B (zh) * | 2010-07-09 | 2013-04-17 | 中国科学院长春光学精密机械与物理研究所 | 基于力矩输出能力最优的单框架控制力矩陀螺操纵方法 |
WO2012009198A2 (en) * | 2010-07-14 | 2012-01-19 | University Of Florida Research Foundation, Inc. | System and method for assessing the performance of an attitude control system for small satellites |
ITTO20131067A1 (it) * | 2013-12-23 | 2015-06-24 | Thales Alenia Space Italia S P A C On Unico Socio | Sistema di controllo di assetto per applicazioni satellitari agili |
-
2013
- 2013-12-23 IT IT001067A patent/ITTO20131067A1/it unknown
-
2014
- 2014-12-23 KR KR1020167020155A patent/KR102266872B1/ko active IP Right Grant
- 2014-12-23 CN CN201480070640.8A patent/CN106068440B/zh active Active
- 2014-12-23 EP EP17168876.5A patent/EP3216705B1/en active Active
- 2014-12-23 SG SG11201604913TA patent/SG11201604913TA/en unknown
- 2014-12-23 BR BR112016014819A patent/BR112016014819A2/pt not_active Application Discontinuation
- 2014-12-23 EA EA201691308A patent/EA201691308A1/ru unknown
- 2014-12-23 MX MX2016008286A patent/MX2016008286A/es unknown
- 2014-12-23 CN CN201910639332.7A patent/CN110329550B/zh active Active
- 2014-12-23 US US15/107,419 patent/US10703511B2/en active Active
- 2014-12-23 EP EP14828539.8A patent/EP3087006B1/en active Active
- 2014-12-23 ES ES14828539.8T patent/ES2694691T3/es active Active
- 2014-12-23 PL PL14828539T patent/PL3087006T3/pl unknown
- 2014-12-23 SG SG10201805372WA patent/SG10201805372WA/en unknown
- 2014-12-23 AU AU2014372139A patent/AU2014372139B2/en not_active Ceased
- 2014-12-23 WO PCT/IB2014/067282 patent/WO2015097672A2/en active Application Filing
- 2014-12-23 EA EA201891068A patent/EA201891068A1/ru unknown
-
2018
- 2018-02-01 AU AU2018200772A patent/AU2018200772A1/en not_active Abandoned
-
2019
- 2019-10-17 US US16/656,257 patent/US20200047922A1/en not_active Abandoned
Also Published As
Publication number | Publication date |
---|---|
ES2694691T3 (es) | 2018-12-26 |
CN106068440A (zh) | 2016-11-02 |
WO2015097672A2 (en) | 2015-07-02 |
EP3216705B1 (en) | 2019-01-30 |
US20200047922A1 (en) | 2020-02-13 |
ITTO20131067A1 (it) | 2015-06-24 |
EP3087006A2 (en) | 2016-11-02 |
SG11201604913TA (en) | 2016-07-28 |
AU2018200772A1 (en) | 2018-02-22 |
PL3087006T3 (pl) | 2019-01-31 |
AU2014372139B2 (en) | 2018-02-22 |
AU2014372139A1 (en) | 2016-07-07 |
WO2015097672A3 (en) | 2015-10-29 |
EA201691308A1 (ru) | 2016-11-30 |
CN106068440B (zh) | 2019-08-09 |
EA201891068A1 (ru) | 2019-03-29 |
US20170029139A1 (en) | 2017-02-02 |
SG10201805372WA (en) | 2018-08-30 |
EP3216705A1 (en) | 2017-09-13 |
CN110329550B (zh) | 2022-09-06 |
MX2016008286A (es) | 2017-01-09 |
US10703511B2 (en) | 2020-07-07 |
KR20160125357A (ko) | 2016-10-31 |
EP3087006B1 (en) | 2018-08-29 |
KR102266872B1 (ko) | 2021-06-21 |
CN110329550A (zh) | 2019-10-15 |
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Legal Events
Date | Code | Title | Description |
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B06U | Preliminary requirement: requests with searches performed by other patent offices: procedure suspended [chapter 6.21 patent gazette] | ||
B11B | Dismissal acc. art. 36, par 1 of ipl - no reply within 90 days to fullfil the necessary requirements |