JP4307247B2 - ジャイロダインのクラスターによって人工衛星の姿勢を制御しかつ操舵するための方法及び装置 - Google Patents

ジャイロダインのクラスターによって人工衛星の姿勢を制御しかつ操舵するための方法及び装置 Download PDF

Info

Publication number
JP4307247B2
JP4307247B2 JP2003507644A JP2003507644A JP4307247B2 JP 4307247 B2 JP4307247 B2 JP 4307247B2 JP 2003507644 A JP2003507644 A JP 2003507644A JP 2003507644 A JP2003507644 A JP 2003507644A JP 4307247 B2 JP4307247 B2 JP 4307247B2
Authority
JP
Japan
Prior art keywords
actuators
satellite
angular momentum
attitude
gimbal
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.)
Expired - Lifetime
Application number
JP2003507644A
Other languages
English (en)
Japanese (ja)
Other versions
JP2004535324A5 (enExample
JP2004535324A (ja
Inventor
クリステン・ラガデック
アンジュ・デファンディーニ
ジュリアン・モラン
Original Assignee
ウアデエス・アストリウム・サ
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 ウアデエス・アストリウム・サ filed Critical ウアデエス・アストリウム・サ
Publication of JP2004535324A publication Critical patent/JP2004535324A/ja
Publication of JP2004535324A5 publication Critical patent/JP2004535324A5/ja
Application granted granted Critical
Publication of JP4307247B2 publication Critical patent/JP4307247B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Automation & Control Theory (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Radio Relay Systems (AREA)
JP2003507644A 2001-06-26 2002-06-24 ジャイロダインのクラスターによって人工衛星の姿勢を制御しかつ操舵するための方法及び装置 Expired - Lifetime JP4307247B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0108409A FR2826470B1 (fr) 2001-06-26 2001-06-26 Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes
PCT/FR2002/002181 WO2003001311A1 (fr) 2001-06-26 2002-06-24 Procede et dispositif de pilotage de l'attitude et de guidage d'un satellite par grappe de gyrodynes

Publications (3)

Publication Number Publication Date
JP2004535324A JP2004535324A (ja) 2004-11-25
JP2004535324A5 JP2004535324A5 (enExample) 2008-11-13
JP4307247B2 true JP4307247B2 (ja) 2009-08-05

Family

ID=8864776

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003507644A Expired - Lifetime JP4307247B2 (ja) 2001-06-26 2002-06-24 ジャイロダインのクラスターによって人工衛星の姿勢を制御しかつ操舵するための方法及び装置

Country Status (10)

Country Link
US (1) US7171290B2 (enExample)
EP (1) EP1407335B1 (enExample)
JP (1) JP4307247B2 (enExample)
AT (1) ATE341783T1 (enExample)
CA (1) CA2452250C (enExample)
DE (1) DE60215174T2 (enExample)
ES (1) ES2274088T3 (enExample)
FR (1) FR2826470B1 (enExample)
IL (2) IL159573A0 (enExample)
WO (1) WO2003001311A1 (enExample)

Families Citing this family (55)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2846107B1 (fr) * 2002-10-21 2005-06-24 Cit Alcatel Dispositif de controle d'attitude d'un satellite geostationnaire
FR2850948B1 (fr) 2003-02-07 2006-01-06 Astrium Sas Dispositif de pilotage de l'attitude d'un satellite par actionneurs gyroscopiques
US7252667B2 (en) 2003-11-19 2007-08-07 Sherwood Services Ag Open vessel sealing instrument with cutting mechanism and distal lockout
US7246776B2 (en) * 2004-07-23 2007-07-24 Honeywell International, Inc. Method and system for CMG array singularity avoidance
US7464899B2 (en) * 2005-08-03 2008-12-16 Honeywell International Inc. Method and system for determining a singularity free momentum path
US7370833B2 (en) * 2005-10-20 2008-05-13 Honeywell International Inc. Method and system for determining a singularity free momentum path
US7693619B2 (en) 2005-11-30 2010-04-06 Honeywell International Inc. Method and system for controlling sets of collinear control moment gyroscopes with offset determination without attitude trajectory of spacecraft
US7805226B2 (en) 2006-09-29 2010-09-28 Honeywell International Inc. Hierarchical strategy for singularity avoidance in arrays of control moment gyroscopes
FR2907423B1 (fr) 2006-10-23 2009-07-03 Astrium Sas Soc Par Actions Si Gyrodyne et son dispositif de montage
EP2123772A1 (en) 2008-04-29 2009-11-25 DSM IP Assets B.V. Beta-lactam antibiotic producing strains
CN102131921A (zh) 2008-08-05 2011-07-20 帝斯曼知识产权资产管理有限公司 生产己二酰基-7-adca的菌株
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
US8209070B2 (en) * 2008-12-17 2012-06-26 Honeywell International Inc. Methods and systems for efficiently orienting an agile vehicle using a gyroscope array
WO2010122141A1 (en) 2009-04-24 2010-10-28 Dsm Ip Assets B.V. Carbohydrate degrading polypeptide and uses thereof
US9199746B2 (en) 2009-05-19 2015-12-01 University Of Florida Research Foundation, Inc. Attitude control system for small satellites
US8014911B2 (en) * 2009-11-03 2011-09-06 Honeywell International Inc. Methods and systems for imposing a momentum boundary while reorienting an agile vehicle with control moment gyroscopes
CN102834511A (zh) 2010-02-11 2012-12-19 帝斯曼知识产权资产管理有限公司 具有纤维二糖水解酶活性的多肽及其用途
US8346538B2 (en) 2010-05-25 2013-01-01 Honeywell International Inc. Methods and systems for reducing angular velocity using a gyroscope array
BR112012033701A2 (pt) 2010-06-29 2018-08-28 Dsm Ip Assets Bv polipeptídeo tendo atividade de degradação de carbohidrato e seus usos
CN103180337A (zh) 2010-06-29 2013-06-26 帝斯曼知识产权资产管理有限公司 具有膨胀因子活性的多肽及其用途
CN102971419B (zh) 2010-06-29 2015-02-11 帝斯曼知识产权资产管理有限公司 具有降解碳水化合物材料的活性或帮助降解碳水化合物材料的活性的多肽及其用途
CA2803982A1 (en) 2010-06-29 2012-01-05 Dsm Ip Assets B.V. Polypeptide having beta-glucosidase activity and uses thereof
CN103391999B (zh) 2010-06-29 2016-06-22 帝斯曼知识产权资产管理有限公司 具有乙酰基木聚糖酯酶活性的多肽及其用途
US9121013B2 (en) 2010-06-29 2015-09-01 Dsm Ip Assets B.V. Polypeptide having beta-glucosidase activity and uses thereof
JP5556782B2 (ja) * 2011-10-04 2014-07-23 三菱電機株式会社 人工衛星の姿勢制御装置
FR2981050B1 (fr) * 2011-10-07 2014-07-25 Larminat Philippe De Commande d'actionneur gyroscopique par formulation directe, pour pilotage d'attitude de satellite agile
CN102566578B (zh) * 2012-01-12 2013-06-19 北京航空航天大学 基于奇异值分解的单框架控制力矩陀螺群协调控制方法
US10052848B2 (en) 2012-03-06 2018-08-21 Apple Inc. Sapphire laminates
US9221289B2 (en) 2012-07-27 2015-12-29 Apple Inc. Sapphire window
CN103064392B (zh) * 2012-12-28 2015-05-27 中国人民解放军国防科学技术大学 星载综合电子系统
US9232672B2 (en) 2013-01-10 2016-01-05 Apple Inc. Ceramic insert control mechanism
EP3447136B1 (en) 2013-02-04 2020-05-13 DSM IP Assets B.V. Carbohydrate degrading polypeptide and uses thereof
WO2014202622A2 (en) 2013-06-19 2014-12-24 Dsm Ip Assets B.V. Rasamsonia gene and use thereof
WO2014202620A2 (en) 2013-06-19 2014-12-24 Dsm Ip Assets B.V. Rasamsonia gene and use thereof
WO2014202624A2 (en) 2013-06-19 2014-12-24 Dsm Ip Assets B.V. Rasamsonia gene and use thereof
WO2014202621A1 (en) 2013-06-20 2014-12-24 Dsm Ip Assets B.V. Carbohydrate degrading polypeptide and uses thereof
US9632537B2 (en) 2013-09-23 2017-04-25 Apple Inc. Electronic component embedded in ceramic material
US9678540B2 (en) 2013-09-23 2017-06-13 Apple Inc. Electronic component embedded in ceramic material
US9154678B2 (en) 2013-12-11 2015-10-06 Apple Inc. Cover glass arrangement for an electronic device
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
US9225056B2 (en) 2014-02-12 2015-12-29 Apple Inc. Antenna on sapphire structure
CN104460427B (zh) * 2014-10-31 2017-01-25 上海卫星工程研究所 模块化微型卫星平台综合电子系统
CN104527994B (zh) * 2015-01-21 2016-08-24 哈尔滨工业大学 异面交叉快变轨道固定时间稳定姿态指向跟踪控制方法
KR101654282B1 (ko) * 2015-02-13 2016-09-05 홍대안 다중 모멘텀 휠 어셈블리를 적용한 제어 모멘트 자이로
JP6373496B2 (ja) 2015-06-22 2018-08-15 三菱電機株式会社 宇宙機の姿勢制御装置およびｃｍｇのジンバル角演算方法
FR3038082B1 (fr) * 2015-06-24 2017-07-07 Centre Nat D'etudes Spatiales (Cnes) Procede d'evitement d'une zone interdite par un satellite
US10406634B2 (en) 2015-07-01 2019-09-10 Apple Inc. Enhancing strength in laser cutting of ceramic components
KR101788577B1 (ko) 2016-03-23 2017-10-23 이동주 볼 로봇을 이용한 탑승형 이동장치의 제어방법
WO2017211930A1 (en) 2016-06-10 2017-12-14 Dsm Ip Assets B.V. Mutant lipase and use thereof
CN106020224B (zh) * 2016-07-22 2019-01-08 北京航空航天大学 一种考虑质心位置不确定性的上面级矢量推力控制方法
KR20210013585A (ko) 2018-05-18 2021-02-04 디에스엠 아이피 어셋츠 비.브이. 돌연변이체 리파아제 및 이의 용도
CA3100615A1 (en) 2018-05-18 2019-11-21 Dsm Ip Assets B.V. Mutant lipase and use thereof
CN110723316B (zh) * 2019-09-16 2020-09-18 北京控制工程研究所 一种sgcmg的框架角速度确定方法
CN112455726B (zh) * 2020-12-10 2022-04-19 长光卫星技术股份有限公司 一种低轨光学遥感卫星多点成像快速机动控制方法
CN117734969B (zh) * 2023-12-19 2024-08-20 北京航空航天大学 一种基于单框架控制力矩陀螺的电推进装置推力反演方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3741500A (en) * 1971-04-21 1973-06-26 Sperry Rand Corp A cmg fine attitude control system
FR2773775B1 (fr) 1998-01-20 2000-03-24 Matra Marconi Space France Actionneur gyroscopique
US6131056A (en) * 1998-03-16 2000-10-10 Honeywell International Inc. Continuous attitude control that avoids CMG array singularities
FR2786283B1 (fr) * 1998-11-19 2001-01-26 Matra Marconi Space France Procede et dispositif de pilotage de l'attitude d'un satellite
US6682019B2 (en) * 2002-04-04 2004-01-27 Honeywell International Inc. Minimum energy wheel configurations for energy storage and attitude control

Also Published As

Publication number Publication date
CA2452250C (fr) 2014-12-23
ES2274088T3 (es) 2007-05-16
EP1407335A1 (fr) 2004-04-14
IL159573A0 (en) 2004-06-01
FR2826470A1 (fr) 2002-12-27
IL159573A (en) 2008-11-03
US20040167683A1 (en) 2004-08-26
FR2826470B1 (fr) 2003-09-19
WO2003001311A1 (fr) 2003-01-03
CA2452250A1 (fr) 2003-01-03
US7171290B2 (en) 2007-01-30
DE60215174T2 (de) 2007-08-23
ATE341783T1 (de) 2006-10-15
EP1407335B1 (fr) 2006-10-04
JP2004535324A (ja) 2004-11-25
DE60215174D1 (de) 2006-11-16

Similar Documents

Publication Publication Date Title
JP4307247B2 (ja) ジャイロダインのクラスターによって人工衛星の姿勢を制御しかつ操舵するための方法及び装置
JP2004535324A5 (enExample)
EP1064591B1 (en) Continuous spacecraft attitude control that avoids cmg array singularities
Kurokawa Constrained steering law of pyramid-type control moment gyros and ground tests
US6039290A (en) Robust singularity avoidance in satellite attitude control
US6917862B2 (en) Singularity escape/avoidance steering logic for control moment gyro systems
US7904214B2 (en) Singularity escape and avoidance using a virtual array rotation
US6154691A (en) Orienting a satellite with controlled momentum gyros
JPH06510502A (ja) ３軸安定衛星の姿勢制御で使用する測定装置と付属する評価方法、制御系および制御方法
Takada et al. Control moment gyro singularity-avoidance steering control based on singular-surface cost function
JP2003521424A (ja) 宇宙船の姿勢を制御するシステムおよび方法
JP4249901B2 (ja) 衛星の姿勢制御のための各運動量に基づくｃｍｇ制御
Kojima Singularity analysis and steering control laws for adaptive-skew pyramid-type control moment gyros
Ivanov et al. Decentralized differential drag based control of nanosatellites swarm spatial distribution using magnetorquers
Lightsey et al. Flight results of GPS based attitude control on the REX II spacecraft
CN110697085B (zh) 一种双sgcmg与磁力矩器组合的卫星控制方法
US7370833B2 (en) Method and system for determining a singularity free momentum path
Maghami et al. Laser interferometer space antenna dynamics and controls model
Saberi et al. Design and analysis of gimbal thruster configurations for 3-axis satellite attitude control
Reijneveld et al. Attitude control system of the Delfi-n3Xt satellite
Ninomiya et al. Magnetic torquing scheme for attitude control of a wheel-stabilized astronomy satellite
Merrill et al. Lyapunov-based Two-Axis Magnetic Attitude Control of a Rigid Spacecraft
JPH06144398A (ja) 人工衛星の姿勢制御装置
Pecora et al. Robust Attitude Control Using Electrospray Thrusters
Takada et al. Receding horizon control on steering of control moment gyro for fast attitude maneuver

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20050617

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20070918

A601 Written request for extension of time

Free format text: JAPANESE INTERMEDIATE CODE: A601

Effective date: 20071207

A602 Written permission of extension of time

Free format text: JAPANESE INTERMEDIATE CODE: A602

Effective date: 20071214

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20080318

A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20080520

A524 Written submission of copy of amendment under article 19 pct

Free format text: JAPANESE INTERMEDIATE CODE: A524

Effective date: 20080917

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20080925

A911 Transfer to examiner for re-examination before appeal (zenchi)

Free format text: JAPANESE INTERMEDIATE CODE: A911

Effective date: 20081007

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A821

Effective date: 20080918

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20090331

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20090428

R150 Certificate of patent or registration of utility model

Ref document number: 4307247

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20120515

Year of fee payment: 3

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20130515

Year of fee payment: 4

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

EXPY Cancellation because of completion of term