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ITTO20131067A1 - Sistema di controllo di assetto per applicazioni satellitari agili - Google Patents

Sistema di controllo di assetto per applicazioni satellitari agili

Info

Publication number
ITTO20131067A1
ITTO20131067A1 IT001067A ITTO20131067A ITTO20131067A1 IT TO20131067 A1 ITTO20131067 A1 IT TO20131067A1 IT 001067 A IT001067 A IT 001067A IT TO20131067 A ITTO20131067 A IT TO20131067A IT TO20131067 A1 ITTO20131067 A1 IT TO20131067A1
Authority
IT
Italy
Prior art keywords
control system
trimming control
satellite applications
agile satellite
agile
Prior art date
Application number
IT001067A
Other languages
English (en)
Inventor
Marco Anania
Domenico Cascone
Original Assignee
Thales Alenia Space Italia S P A C On 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 S P A C On Unico Socio filed Critical Thales Alenia Space Italia S P A C On Unico Socio
Priority to IT001067A priority Critical patent/ITTO20131067A1/it
Priority to EP14828539.8A priority patent/EP3087006B1/en
Priority to BR112016014819A priority patent/BR112016014819A2/pt
Priority to CN201910639332.7A priority patent/CN110329550B/zh
Priority to SG11201604913TA priority patent/SG11201604913TA/en
Priority to EA201891068A priority patent/EA201891068A1/ru
Priority to PL14828539T priority patent/PL3087006T3/pl
Priority to PCT/IB2014/067282 priority patent/WO2015097672A2/en
Priority to EP17168876.5A priority patent/EP3216705B1/en
Priority to ES14828539.8T priority patent/ES2694691T3/es
Priority to AU2014372139A priority patent/AU2014372139B2/en
Priority to CN201480070640.8A priority patent/CN106068440B/zh
Priority to US15/107,419 priority patent/US10703511B2/en
Priority to SG10201805372WA priority patent/SG10201805372WA/en
Priority to KR1020167020155A priority patent/KR102266872B1/ko
Priority to EA201691308A priority patent/EA201691308A1/ru
Priority to MX2016008286A priority patent/MX2016008286A/es
Publication of ITTO20131067A1 publication Critical patent/ITTO20131067A1/it
Priority to AU2018200772A priority patent/AU2018200772A1/en
Priority to US16/656,257 priority patent/US20200047922A1/en

Links

Classifications

    • 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
    • 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
    • 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
    • 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)
IT001067A 2013-12-23 2013-12-23 Sistema di controllo di assetto per applicazioni satellitari agili ITTO20131067A1 (it)

Priority Applications (19)

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
ES14828539.8T ES2694691T3 (es) 2013-12-23 2014-12-23 Control de posición para aplicaciones ágiles de satélite
AU2014372139A AU2014372139B2 (en) 2013-12-23 2014-12-23 Attitude control for agile satellite applications
CN201910639332.7A CN110329550B (zh) 2013-12-23 2014-12-23 用于敏捷卫星应用的姿态控制
SG11201604913TA SG11201604913TA (en) 2013-12-23 2014-12-23 Attitude control for agile satellite applications
EA201891068A EA201891068A1 (ru) 2013-12-23 2014-12-23 Управление пространственным положением для маневренных спутниковых приборов
PL14828539T PL3087006T3 (pl) 2013-12-23 2014-12-23 Kontrola położenia dla sprawnych zastosowań satelity
PCT/IB2014/067282 WO2015097672A2 (en) 2013-12-23 2014-12-23 Attitude control for agile satellite applications
EP17168876.5A EP3216705B1 (en) 2013-12-23 2014-12-23 Attitude control for agile satellite applications
EP14828539.8A EP3087006B1 (en) 2013-12-23 2014-12-23 Attitude control for agile satellite applications
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
CN201480070640.8A CN106068440B (zh) 2013-12-23 2014-12-23 用于敏捷卫星应用的姿态控制
US15/107,419 US10703511B2 (en) 2013-12-23 2014-12-23 Attitude control for agile satellite applications
SG10201805372WA SG10201805372WA (en) 2013-12-23 2014-12-23 Attitude control for agile satellite applications
KR1020167020155A KR102266872B1 (ko) 2013-12-23 2014-12-23 애자일 위성 어플리케이션들을 위한 자세 제어
EA201691308A EA201691308A1 (ru) 2013-12-23 2014-12-23 Управление пространственным положением для маневренных спутниковых приборов
MX2016008286A MX2016008286A (es) 2013-12-23 2014-12-23 Control de actitud para aplicaciones de satelites agiles.
AU2018200772A AU2018200772A1 (en) 2013-12-23 2018-02-01 Attitude control for agile satellite applications
US16/656,257 US20200047922A1 (en) 2013-12-23 2019-10-17 Attitude Control for Agile Satellite Applications

Applications Claiming Priority (1)

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

Publications (1)

Publication Number Publication Date
ITTO20131067A1 true ITTO20131067A1 (it) 2015-06-24

Family

ID=50116102

Family Applications (1)

Application Number Title Priority Date Filing Date
IT001067A ITTO20131067A1 (it) 2013-12-23 2013-12-23 Sistema di controllo di assetto per applicazioni satellitari agili

Country Status (13)

Country Link
US (2) US10703511B2 (it)
EP (2) EP3216705B1 (it)
KR (1) KR102266872B1 (it)
CN (2) CN110329550B (it)
AU (2) AU2014372139B2 (it)
BR (1) BR112016014819A2 (it)
EA (2) EA201691308A1 (it)
ES (1) ES2694691T3 (it)
IT (1) ITTO20131067A1 (it)
MX (1) MX2016008286A (it)
PL (1) PL3087006T3 (it)
SG (2) SG11201604913TA (it)
WO (1) WO2015097672A2 (it)

Cited By (1)

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CN117330049A (zh) * 2023-11-27 2024-01-02 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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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
CN114955011B (zh) * 2022-04-12 2024-10-18 北京航空航天大学 一种dgvscmg飞轮模式下框架系统定角控制方法

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US20030160132A1 (en) * 2002-02-22 2003-08-28 Osterberg David A. Dynamic unbalance compensation system and method
EP1908686A1 (en) * 2006-09-29 2008-04-09 Honeywell International Inc. Hierarchial strategy for singularity avoidance in arrays of control moment gyroscopes
US20110011982A1 (en) * 2009-07-20 2011-01-20 Jason Herman Modular control moment gyroscope (cmg) system for spacecraft attitude control

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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
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
US8020809B2 (en) 2007-04-18 2011-09-20 Ithaco Space Systems, Inc. Direct torque actuator control for control moment gyroscope
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US9199746B2 (en) * 2009-05-19 2015-12-01 University Of Florida Research Foundation, Inc. Attitude control system for small satellites
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
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US20030160132A1 (en) * 2002-02-22 2003-08-28 Osterberg David A. Dynamic unbalance compensation system and method
EP1908686A1 (en) * 2006-09-29 2008-04-09 Honeywell International Inc. Hierarchial strategy for singularity avoidance in arrays of control moment gyroscopes
US20110011982A1 (en) * 2009-07-20 2011-01-20 Jason Herman Modular control moment gyroscope (cmg) system for spacecraft attitude control

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LAPPAS V ET AL: "DESIGN AND TESTING OF A CONTROL MOMENT GYROSCOPE CLUSTER FOR SMALL SATELLITES", JOURNAL OF SPACECRAFT AND ROCKETS, AMERICAN INSTITUTE OF AERONAUTICS AND ASTRONAUTICS,REASTON,VA, US, vol. 42, no. 4, 1 July 2005 (2005-07-01), pages 729 - 739, XP001234352, ISSN: 0022-4650 *

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN117330049A (zh) * 2023-11-27 2024-01-02 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
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

Also Published As

Publication number Publication date
AU2014372139B2 (en) 2018-02-22
WO2015097672A2 (en) 2015-07-02
EP3087006B1 (en) 2018-08-29
KR20160125357A (ko) 2016-10-31
US20200047922A1 (en) 2020-02-13
AU2014372139A1 (en) 2016-07-07
EP3216705B1 (en) 2019-01-30
SG11201604913TA (en) 2016-07-28
US20170029139A1 (en) 2017-02-02
US10703511B2 (en) 2020-07-07
ES2694691T3 (es) 2018-12-26
WO2015097672A3 (en) 2015-10-29
CN106068440B (zh) 2019-08-09
AU2018200772A1 (en) 2018-02-22
CN110329550B (zh) 2022-09-06
MX2016008286A (es) 2017-01-09
CN106068440A (zh) 2016-11-02
BR112016014819A2 (pt) 2017-08-08
EA201691308A1 (ru) 2016-11-30
PL3087006T3 (pl) 2019-01-31
EP3216705A1 (en) 2017-09-13
SG10201805372WA (en) 2018-08-30
KR102266872B1 (ko) 2021-06-21
EA201891068A1 (ru) 2019-03-29
CN110329550A (zh) 2019-10-15
EP3087006A2 (en) 2016-11-02

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