ES2025796T3 - Dispositivo y procedimiento de apuntado de una sonda espacial hacia un cuerpo celeste. - Google Patents

Dispositivo y procedimiento de apuntado de una sonda espacial hacia un cuerpo celeste.

Info

Publication number
ES2025796T3
ES2025796T3 ES198888401233T ES88401233T ES2025796T3 ES 2025796 T3 ES2025796 T3 ES 2025796T3 ES 198888401233 T ES198888401233 T ES 198888401233T ES 88401233 T ES88401233 T ES 88401233T ES 2025796 T3 ES2025796 T3 ES 2025796T3
Authority
ES
Spain
Prior art keywords
pointing
procedure
probe
axis
celestial body
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
ES198888401233T
Other languages
English (en)
Inventor
Denis Moura
Louis Torres
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.)
Centre National dEtudes Spatiales CNES
Original Assignee
Centre National dEtudes Spatiales CNES
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 Centre National dEtudes Spatiales CNES filed Critical Centre National dEtudes Spatiales CNES
Application granted granted Critical
Publication of ES2025796T3 publication Critical patent/ES2025796T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

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
    • B64G1/36—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
    • 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

Abstract

DISPOSITIVO Y PROCEDIMIENTO DE APUNTE DE UNA SONDA ESPECIAL HACIA UN CUERPO CELESTE. EL DISPOSITIVO COMPRENDE UN VELAMEN O PARED SOLAR (30) QUE PRESENTA UNA DIS - SIMETRIA ALREDEDOR DE UN EJE (Z) Y QUE SOMETE A LA SONDA (S) A UN ACOPLAMIENTO DE BASCULAMIENTO DE PRESION SOLAR. UNA RUEDA CINETICA (20) GIRA ALREDEDOR DE UN EJE (X), QUE PRODUCE UNA ROTACION DE LA SONDA ALREDEDOR DEL EJE PERPENDICULAR A LOS DOS PRECEDENTES (Y). LA VELOCIDAD DE ROTACION DE LA RUEDA (20) SE VARIA POR UN SISTEMA DE COMANDO (23, 24) A FIN DE MODIFICAR LA VELOCIDAD DE ROTACION DE LA SONDA. APLICACION EN LAS SONDAS ESPECIALES QUE EVOLUCIONAN EN EL PLANO DE LA ECLIPTICA.
ES198888401233T 1987-05-22 1988-05-20 Dispositivo y procedimiento de apuntado de una sonda espacial hacia un cuerpo celeste. Expired - Lifetime ES2025796T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR8707221A FR2615477B1 (fr) 1987-05-22 1987-05-22 Dispositif et procede de pointage d'une sonde spatiale vers un corps celeste

Publications (1)

Publication Number Publication Date
ES2025796T3 true ES2025796T3 (es) 1992-04-01

Family

ID=9351356

Family Applications (1)

Application Number Title Priority Date Filing Date
ES198888401233T Expired - Lifetime ES2025796T3 (es) 1987-05-22 1988-05-20 Dispositivo y procedimiento de apuntado de una sonda espacial hacia un cuerpo celeste.

Country Status (7)

Country Link
US (1) US4909460A (es)
EP (1) EP0295978B1 (es)
AT (1) ATE66191T1 (es)
DE (1) DE3864201D1 (es)
ES (1) ES2025796T3 (es)
FR (1) FR2615477B1 (es)
GR (1) GR3002666T3 (es)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2630705B1 (fr) * 1988-04-28 1990-08-24 Rhone Poulenc Sa Procede d'observation par balayage d'un corps celeste et de mesure d'une vitesse angulaire d'un vehicule spatial, systeme d'observation pour sa mise en oeuvre, et vehicule spatial le comportant
US4949922A (en) * 1988-12-09 1990-08-21 Hughes Aircraft Company Satellite control system
US5012992A (en) * 1988-12-09 1991-05-07 Hughes Aircraft Company Spin stabilization via momentum wheels or similar devices
FR2648782B1 (fr) * 1989-06-23 1991-10-18 Aerospatiale Systeme de controle d'attitude de satellite utilisant une boucle magnetique supraconductrice
US5092543A (en) * 1989-09-27 1992-03-03 General Electric Company Spacecraft attitude control with avoidance constraint
FR2655167B1 (fr) * 1989-11-29 1992-04-03 Aerospatiale Procede de controle d'attitude en roulis et en lacet d'un satellite.
US5080307A (en) * 1990-05-14 1992-01-14 Hughes Aircraft Company Spacecraft earth-pointing attitude acquisition method
FR2669887B1 (fr) * 1990-11-30 1995-06-02 Aerospatiale Procede de controle d'attitude en tangage d'un satellite grace a la pression de radiation solaire et satellite adapte a sa mise en óoeuvre.
DE4114804A1 (de) * 1991-05-07 1992-11-12 Messerschmitt Boelkow Blohm Vorrichtung zur lageregelung von satelliten mit solardruckmomenten
US5337981A (en) * 1991-11-27 1994-08-16 Hughes Aircraft Company Method and apparatus for compensating for solar torque transients on a satellite during a solar eclipse
US5310144A (en) * 1992-07-06 1994-05-10 Hughes Aircraft Company Method and apparatus for satellite torque balancing
DE10114085C1 (de) * 2001-03-22 2002-07-25 Astrium Gmbh Verfahren zum Betrieb eines rotierenden Raumfahrzeugs mit variierender Rotation
KR100573876B1 (ko) * 2004-07-13 2006-04-25 한국과학기술원 태양 복사 압력을 이용하여 타원 궤도에 있는 위성 자세제어 방법
CN115042995B (zh) * 2022-06-10 2022-11-18 北京航天飞行控制中心 地外天体分离探头释放分离规划方法、装置、设备及介质

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1413658A (en) * 1972-03-20 1975-11-12 Rca Corp Solar torque compensation for a satellite or other spacecraft
FR2530046A1 (fr) * 1982-07-06 1984-01-13 Matra Procede et dispositif de commande d'attitude pour satellite geosynchrone
FR2531547A1 (fr) * 1982-08-03 1984-02-10 Europ Agence Spatiale Systeme de controle d'attitude d'un satellite geostationnaire
FR2580582B1 (fr) * 1985-04-19 1987-06-26 Matra Procede et dispositif d'amortissement de nutation de satellite par commande d'orientation de masses presentant un produit d'inertie variable
US4767084A (en) * 1986-09-18 1988-08-30 Ford Aerospace & Communications Corporation Autonomous stationkeeping for three-axis stabilized spacecraft

Also Published As

Publication number Publication date
EP0295978B1 (fr) 1991-08-14
FR2615477A1 (fr) 1988-11-25
FR2615477B1 (fr) 1989-08-18
US4909460A (en) 1990-03-20
GR3002666T3 (en) 1993-01-25
ATE66191T1 (de) 1991-08-15
DE3864201D1 (de) 1991-09-19
EP0295978A1 (fr) 1988-12-21

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