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ES2047695T3 - Procedimiento y sistema de control autonomo de la orbita de un satelite geoestacionario. - Google Patents

Procedimiento y sistema de control autonomo de la orbita de un satelite geoestacionario.

Info

Publication number
ES2047695T3
ES2047695T3 ES89402567T ES89402567T ES2047695T3 ES 2047695 T3 ES2047695 T3 ES 2047695T3 ES 89402567 T ES89402567 T ES 89402567T ES 89402567 T ES89402567 T ES 89402567T ES 2047695 T3 ES2047695 T3 ES 2047695T3
Authority
ES
Spain
Prior art keywords
satellite
alpha
procedure
vector
orbit
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
ES89402567T
Other languages
English (en)
Inventor
Patrick Aime Alexandre Maute
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Group SAS
Original Assignee
Airbus Group SAS
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 Airbus Group SAS filed Critical Airbus Group SAS
Application granted granted Critical
Publication of ES2047695T3 publication Critical patent/ES2047695T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C21/00—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00
    • G01C21/24—Navigation; Navigational instruments not provided for in groups G01C1/00 - G01C19/00 specially adapted for cosmonautical navigation
    • 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
    • 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
    • B64G1/244—Spacecraft control systems
    • B64G1/245—Attitude control algorithms for spacecraft attitude control
    • 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • 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
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/361—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using star sensors
    • 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/363—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using sun sensors
    • 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
    • B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
    • B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Physics & Mathematics (AREA)
  • Astronomy & Astrophysics (AREA)
  • General Physics & Mathematics (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)

Abstract

PROCEDIMIENTO PARA EL MANTENIMIENTO EN SU PUESTO DE UN SATELITE EN ORBITA GEOESTACIONARIA, CARACTERIZADO PORQUE: SE DETERMINA EN EL MISMO INSTANTE EL ANGULO (ALFA)1 ENTRE LA DIRECCION (SATELITE-SOL) Y LA DIRECCION (SATELITE-TIERRA), Y EL ANGULO (ALFA)2 ENTRE LA DIRECCION (SATELITE-ESTRELLA POLAR) Y LA DIRECCION (SATELITE-TIERRA); SE DEDUCE EL VECTOR DE ESTADO E FORMADO CON PARAMETROS ORBITALES POR LA FORMULA: Z = H.E + C.B., DONDE Z ES UN VECTOR DE MEDICION CUYOS COMPONENTES ESTAN DEDUCIDOS DE LOS ANGULOS (ALFA)1 Y (ALFA)2, H ES UNA MATRIZ DE MEDICION, C ES UNA MATRIZ DE SENSIBILIDAD A LAS INCLINACIONES, B ES UN VECTOR DE INCLINACION DETERMINADO POR COMPARACION ENTRE EL VECTOR Z MEDIDO Y LAS MEDICIONES HECHAS EN EL SUELO; SE DETERMINA EN CONSECUENCIA Y SE APLICA MEDIANTE UNAS TOBERAS DE MANIPULACION PARA MANTENIMIENTO EN SU PUESTO.
ES89402567T 1988-10-06 1989-09-19 Procedimiento y sistema de control autonomo de la orbita de un satelite geoestacionario. Expired - Lifetime ES2047695T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR888813121A FR2637564B1 (fr) 1988-10-06 1988-10-06 Procede et systeme de controle autonome d'orbite d'un satellite geostationnaire

Publications (1)

Publication Number Publication Date
ES2047695T3 true ES2047695T3 (es) 1994-03-01

Family

ID=9370753

Family Applications (1)

Application Number Title Priority Date Filing Date
ES89402567T Expired - Lifetime ES2047695T3 (es) 1988-10-06 1989-09-19 Procedimiento y sistema de control autonomo de la orbita de un satelite geoestacionario.

Country Status (7)

Country Link
US (1) US5108050A (es)
EP (1) EP0363243B1 (es)
JP (1) JP2847302B2 (es)
CA (1) CA2000214C (es)
DE (1) DE68911830T2 (es)
ES (1) ES2047695T3 (es)
FR (1) FR2637564B1 (es)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19703629A1 (de) * 1997-01-31 1998-08-06 Daimler Benz Aerospace Ag Verfahren zur bordautonomen Bestimmung der Position eines Satelliten
US5107434A (en) * 1990-04-19 1992-04-21 General Electric Company Three-axis spacecraft attitude control using polar star sensor
DE69109266T2 (de) * 1990-08-22 1995-08-24 Microcosm Inc Vorrichtung zum halten eines satelliten auf seiner umlaufbahn.
FR2670886B1 (fr) * 1990-12-21 1994-07-01 Aerospatiale Procede de reacquisition d'attitude par reconnaissance d'etoile pour satellite stabilise 3-axes.
FR2670746B1 (fr) * 1990-12-21 1993-04-16 Aerospatiale Systeme de controle d'attitude pour satellite 3-axes,; notamment pour satellite d'observation.
DE4129630A1 (de) * 1991-09-06 1993-05-06 Deutsche Aerospace Ag, 8000 Muenchen, De Messanordnung und regelungssystem zur lageregelung eines dreiachsenstabilisierten satelliten sowie zugehoerige mess- und regelverfahren
US5562266A (en) * 1992-10-29 1996-10-08 Aerospatiale Societe Nationale Industrielle Rate gyro calibration method and apparatus for a three-axis stabilized satellite
FR2697651B1 (fr) * 1992-10-29 1995-02-03 Aerospatiale Procédé et appareil de calibration des gyromètres d'un satellite stabilisé 3-axes.
US5452869A (en) * 1992-12-18 1995-09-26 Hughes Aircraft Company On-board three-axes attitude determination and control system
RU2033949C1 (ru) * 1993-02-09 1995-04-30 Севастиян Дмитриевич Гнатюк Автономная бортовая система управления космического аппарата "гасад"
US5452077A (en) * 1993-12-09 1995-09-19 Hughes Aircraft Company Transient-free method of determining satellite attitude
DE19518617A1 (de) * 1995-05-24 1996-11-28 Daimler Benz Aerospace Ag Dreiachsenstabilisierter, erdorientierter Satellit und zugehöriges Sonnen- und Erdakquisitonsverfahren unter Benutzung eines Magnetometers
US6098929A (en) * 1998-01-28 2000-08-08 Falbel; Gerald Three axis attitude readout system for geosynchronous spacecraft
US6145790A (en) * 1998-09-22 2000-11-14 Hughes Electronics Corporation Attitude determination system and method
DE60032681T2 (de) * 1999-08-13 2007-10-18 Hughes Electronics Corp., El Segundo Umlaufbahnsteuerung eines Raumfahrzeuges bei Rückmeldung der Lage der Umlaufbahn
US6691033B1 (en) * 2000-07-26 2004-02-10 Hughes Electronics Corporation System and method for calibrating inter-star-tracker misalignments in a stellar inertial attitude determination system
US7454272B1 (en) * 2005-08-25 2008-11-18 Raytheon Company Geostationary stationkeeping method
US8174433B1 (en) 2009-02-26 2012-05-08 Raytheon Company Bias estimation and orbit determination
US9091552B2 (en) * 2011-10-25 2015-07-28 The Boeing Company Combined location and attitude determination system and methods
FR2983981B1 (fr) * 2011-12-09 2014-08-22 Thales Sa Procede et systeme de commande d'un ensemble d'au moins deux satellites, concus pour fournir un service sur une orbite geostationnaire, rendant ledit service sur une orbite non-geostationnaire
US9073648B2 (en) * 2013-02-15 2015-07-07 The Boeing Company Star tracker rate estimation with kalman filter enhancement
CN111238567A (zh) * 2020-01-06 2020-06-05 航天恒星科技有限公司 一种卫星在轨健康监控装置
CN112052560B (zh) * 2020-07-30 2024-07-23 上海航天控制技术研究所 一种系统级星载计算机维护模式闭环仿真设计方法
CN112319850B (zh) * 2020-09-30 2022-05-24 中国卫通集团股份有限公司 一种自动实现同步轨道卫星位置保持的方法及装置
CN112526561B (zh) * 2020-11-27 2024-04-23 中国科学院国家天文台 延长地球静止轨道通信卫星两行星历预报时段方法
CN112769466B (zh) * 2020-12-22 2022-08-12 火眼位置数智科技服务有限公司 低轨卫星星座构型保持方法

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3417661A1 (de) * 1983-05-13 1984-11-15 Mitsubishi Denki K.K., Tokio/Tokyo System zur regelung der lage eines kuenstlichen satelliten
US4617634A (en) * 1983-06-28 1986-10-14 Mitsubishi Denki Kabushiki Kaisha Artificial satellite attitude control system
JPS6171300A (ja) * 1984-09-13 1986-04-12 三菱電機株式会社 人工衛星の姿勢角計算装置
FR2583873B1 (fr) * 1985-06-20 1987-09-11 Matra Procede et dispositif d'injection de satellite sur orbite geostationnaire avec stabilisation suivant les trois axes
GB8616385D0 (en) * 1986-07-04 1986-08-13 Marconi Space Systems Ltd Satellite attitude control
FR2605427A1 (fr) * 1986-10-16 1988-04-22 Centre Nat Etd Spatiales Pointage d'une antenne de sonde spatiale vers la terre
GB8809247D0 (en) * 1988-04-20 1988-05-25 British Aerospace Attitude recovery for spacecraft

Also Published As

Publication number Publication date
EP0363243B1 (fr) 1993-12-29
FR2637564B1 (fr) 1994-10-14
US5108050A (en) 1992-04-28
JP2847302B2 (ja) 1999-01-20
DE68911830D1 (de) 1994-02-10
JPH02156312A (ja) 1990-06-15
DE68911830T2 (de) 1994-04-28
EP0363243A1 (fr) 1990-04-11
FR2637564A1 (fr) 1990-04-13
CA2000214A1 (en) 1990-04-06
CA2000214C (en) 1993-12-21

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