SG10201805372WA - Attitude control for agile satellite applications - Google Patents

Attitude control for agile satellite applications

Info

Publication number
SG10201805372WA
SG10201805372WA SG10201805372WA SG10201805372WA SG10201805372WA SG 10201805372W A SG10201805372W A SG 10201805372WA SG 10201805372W A SG10201805372W A SG 10201805372WA SG 10201805372W A SG10201805372W A SG 10201805372WA SG 10201805372W A SG10201805372W A SG 10201805372WA
Authority
SG
Singapore
Prior art keywords
attitude control
attitude
control
present
satellite applications
Prior art date
Application number
SG10201805372WA
Inventor
Marco Anania
Domenico Cascone
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 SG10201805372WA publication Critical patent/SG10201805372WA/en

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

ATTITUDE CONTROL FOR AGILE SATELLITE APPLICATIONS The present invention relates, in general, to attitude control and, in particular, to control of the attitude of a 5 space platform, conveniently of a satellite and/or a spacecraft. In detail, an aspect of the present invention concerns the use, in an attitude control system (100), of several Control Moment Gyroscopes (3,41,42,43,44,61,62,63,64) with limited gimbal 10 revolutions. Moreover, another aspect of the present invention concerns an improved logic for controlling a Control Moment Gyroscope assembly (4,6,120) of an attitude control system (100). 15 Figures 3,11
SG10201805372WA 2013-12-23 2014-12-23 Attitude control for agile satellite applications SG10201805372WA (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
IT001067A ITTO20131067A1 (en) 2013-12-23 2013-12-23 TRIMMING CONTROL SYSTEM FOR AGILE SATELLITE APPLICATIONS

Publications (1)

Publication Number Publication Date
SG10201805372WA true SG10201805372WA (en) 2018-08-30

Family

ID=50116102

Family Applications (2)

Application Number Title Priority Date Filing Date
SG10201805372WA SG10201805372WA (en) 2013-12-23 2014-12-23 Attitude control for agile satellite applications
SG11201604913TA SG11201604913TA (en) 2013-12-23 2014-12-23 Attitude control for agile satellite applications

Family Applications After (1)

Application Number Title Priority Date Filing Date
SG11201604913TA SG11201604913TA (en) 2013-12-23 2014-12-23 Attitude control for agile satellite applications

Country Status (13)

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

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ITTO20131067A1 (en) * 2013-12-23 2015-06-24 Thales Alenia Space Italia S P A C On Unico Socio TRIMMING CONTROL SYSTEM FOR AGILE SATELLITE APPLICATIONS
US11221633B2 (en) * 2016-05-17 2022-01-11 Raytheon Company Gyroscopic attitude control system
CN107089348B (en) * 2017-04-01 2019-04-30 中国空间技术研究院 On-orbit fault game method based on more flexible accessory satellite dynamics optimized Control Modes
US10276997B1 (en) 2017-10-06 2019-04-30 Honeywell International Inc. Wire assembly including clockspring passes
CN109828595A (en) * 2019-01-31 2019-05-31 中国人民解放军国防科技大学 Method for analyzing approaching feasibility of terminal of dead space spacecraft
CN110329548B (en) * 2019-05-24 2023-01-17 中国人民解放军63789部队 Flywheel system reconstruction method under on-orbit rotation bias control of spacecraft
CN110658838B (en) * 2019-09-19 2022-10-28 北京控制工程研究所 Method and system for calculating three-axis maneuvering angular velocity of agile spacecraft in real time
CN110658837B (en) * 2019-09-19 2020-10-23 北京控制工程研究所 Steady reconstruction method under control moment gyro fault condition
CN111897355B (en) * 2020-08-06 2022-09-13 中国科学院微小卫星创新研究院 Satellite attitude maneuver trajectory planning method
CN112061425B (en) * 2020-09-08 2022-04-08 上海航天控制技术研究所 Method for avoiding interference of earth gas light on agile small satellite star sensor
CN114313311B (en) * 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 Topological structure of multi-body allosteric satellite
CN117330049B (en) * 2023-11-27 2024-01-30 中北大学 Cavity internal reflection high-robustness angular velocity sensor based on singular surface and measuring method

Family Cites Families (18)

* Cited by examiner, † Cited by third party
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 (en) 2001-06-26 2003-09-19 Astrium Sas METHOD AND DEVICE FOR STEERING THE ATTITUDE AND GUIDANCE OF A SATELLITE BY A GYRODYNES CLUSTER
US6772978B2 (en) * 2002-02-22 2004-08-10 Honeywell International Inc. Dynamic unbalance compensation system and method
FR2837580B1 (en) * 2002-03-21 2005-06-03 Astrium Sas GYROSCOPIC ACTUATOR FOR PILOTTING THE ATTITUDE OF A SPATIAL VEHICLE
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 (en) * 2008-09-12 2009-12-02 航天东方红卫星有限公司 A kind of spacecraft attitude control system of handling the unusual avoidance of rule
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 (en) * 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 Single frame control moment gyro control method based on moment output capability optimization
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 (en) * 2013-12-23 2015-06-24 Thales Alenia Space Italia S P A C On Unico Socio TRIMMING CONTROL SYSTEM FOR AGILE SATELLITE APPLICATIONS

Also Published As

Publication number Publication date
CN106068440B (en) 2019-08-09
CN106068440A (en) 2016-11-02
WO2015097672A3 (en) 2015-10-29
US20170029139A1 (en) 2017-02-02
ES2694691T3 (en) 2018-12-26
WO2015097672A2 (en) 2015-07-02
EP3087006A2 (en) 2016-11-02
ITTO20131067A1 (en) 2015-06-24
MX2016008286A (en) 2017-01-09
AU2014372139B2 (en) 2018-02-22
EA201691308A1 (en) 2016-11-30
EA201891068A1 (en) 2019-03-29
KR102266872B1 (en) 2021-06-21
AU2014372139A1 (en) 2016-07-07
AU2018200772A1 (en) 2018-02-22
SG11201604913TA (en) 2016-07-28
US20200047922A1 (en) 2020-02-13
KR20160125357A (en) 2016-10-31
CN110329550A (en) 2019-10-15
US10703511B2 (en) 2020-07-07
EP3087006B1 (en) 2018-08-29
BR112016014819A2 (en) 2017-08-08
CN110329550B (en) 2022-09-06
EP3216705A1 (en) 2017-09-13
EP3216705B1 (en) 2019-01-30
PL3087006T3 (en) 2019-01-31

Similar Documents

Publication Publication Date Title
SG10201805372WA (en) Attitude control for agile satellite applications
IL288191A (en) Navigational system with imposed liability constraints
GB2565264B (en) Inertial navigation system
GB2564764A (en) Sonar sensor fusion and model based virtual and augmented reality systems and methods
EP3110695A4 (en) An improved performance and cost global navigation satellite system architecture
EP3195015A4 (en) Gps-aided inertial navigation method and system
EP3610585A4 (en) Super speed satellite system (s4)
GB201610747D0 (en) Inertial Navigation System
GB201521539D0 (en) Inertial navigation system
EP3430432A4 (en) Navigation satellite orbit and low latency clock determination with wide-lane and narrow-lane bias corrections
GB201815730D0 (en) Systems and methods for autonomous drone navigation
GB2576569B (en) Inertial navigation system
IL245319B (en) Nadir/zenith inertial pointing assistance for two-axis gimbals
EP3415867A4 (en) Control moment gyroscope
MX2017008493A (en) Underwater vehicle.
UA118184C2 (en) Space propulsion module having electric and solid-fuel chemical propulsion
EP3430433A4 (en) Navigation satellite orbit and clock determination with low latency clock corrections
EP3634856A4 (en) Attitude stabilization and orbital distribution for small satellites
GB201604556D0 (en) Celestial navigation system
EP3775545A4 (en) Self propelled thrust-producing controlled moment gyroscope
EP2960743A3 (en) Flight vehicle autopilot
SG11202000536WA (en) Three-axis mems gyroscope
EP3680612A4 (en) Gyroscope based on atomic interference
EP3482075A4 (en) Arcjet propulsion systems for spacecraft
LT3334654T (en) Satellites attitude control system