MX2016008286A - Control de actitud para aplicaciones de satelites agiles. - Google Patents

Control de actitud para aplicaciones de satelites agiles.

Info

Publication number
MX2016008286A
MX2016008286A MX2016008286A MX2016008286A MX2016008286A MX 2016008286 A MX2016008286 A MX 2016008286A MX 2016008286 A MX2016008286 A MX 2016008286A MX 2016008286 A MX2016008286 A MX 2016008286A MX 2016008286 A MX2016008286 A MX 2016008286A
Authority
MX
Mexico
Prior art keywords
attitude control
attitude
present
control
satellite applications
Prior art date
Application number
MX2016008286A
Other languages
English (en)
Inventor
Anania Marco
Cascone Domenico
Original Assignee
Thales Alenia Space Italia Spa Con Unico Socio
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 Thales Alenia Space Italia Spa Con Unico Socio filed Critical Thales Alenia Space Italia Spa Con Unico Socio
Publication of MX2016008286A publication Critical patent/MX2016008286A/es

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

Abstract

La presente invención se relaciona, en general, con el control de la actitud y, en particular, con el control de la actitud de una plataforma espacial, convenientemente de un satélite y/o una nave espacial. En detalle, un aspecto de la presente invención concierne al uso, en un sistema de control de actitud (100), de varios Giroscopios de Control de Momento (3,41,42,43,44,61,62,63,6 4) con revoluciones de cardán limitadas. Además, otro aspecto de la presente invención concierne a una lógica mejorada para controlar un conjunto de Giroscopios de Control de Momento (4,6,120) de un sistema de control de actitud (100).
MX2016008286A 2013-12-23 2014-12-23 Control de actitud para aplicaciones de satelites agiles. MX2016008286A (es)

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
MX2016008286A true MX2016008286A (es) 2017-01-09

Family

ID=50116102

Family Applications (1)

Application Number Title Priority Date Filing Date
MX2016008286A MX2016008286A (es) 2013-12-23 2014-12-23 Control de actitud para aplicaciones de satelites agiles.

Country Status (13)

Country Link
US (2) US10703511B2 (es)
EP (2) EP3087006B1 (es)
KR (1) KR102266872B1 (es)
CN (2) CN106068440B (es)
AU (2) AU2014372139B2 (es)
BR (1) BR112016014819A2 (es)
EA (2) EA201891068A1 (es)
ES (1) ES2694691T3 (es)
IT (1) ITTO20131067A1 (es)
MX (1) MX2016008286A (es)
PL (1) PL3087006T3 (es)
SG (2) SG10201805372WA (es)
WO (1) WO2015097672A2 (es)

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* Cited by examiner, † Cited by third party
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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

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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
US9199746B2 (en) * 2009-05-19 2015-12-01 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

Also Published As

Publication number Publication date
CN106068440B (zh) 2019-08-09
CN106068440A (zh) 2016-11-02
WO2015097672A3 (en) 2015-10-29
US20170029139A1 (en) 2017-02-02
ES2694691T3 (es) 2018-12-26
WO2015097672A2 (en) 2015-07-02
EP3087006A2 (en) 2016-11-02
ITTO20131067A1 (it) 2015-06-24
AU2014372139B2 (en) 2018-02-22
EA201691308A1 (ru) 2016-11-30
SG10201805372WA (en) 2018-08-30
EA201891068A1 (ru) 2019-03-29
KR102266872B1 (ko) 2021-06-21
AU2014372139A1 (en) 2016-07-07
AU2018200772A1 (en) 2018-02-22
SG11201604913TA (en) 2016-07-28
US20200047922A1 (en) 2020-02-13
KR20160125357A (ko) 2016-10-31
CN110329550A (zh) 2019-10-15
US10703511B2 (en) 2020-07-07
EP3087006B1 (en) 2018-08-29
BR112016014819A2 (pt) 2017-08-08
CN110329550B (zh) 2022-09-06
EP3216705A1 (en) 2017-09-13
EP3216705B1 (en) 2019-01-30
PL3087006T3 (pl) 2019-01-31

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