IT9020889A0 - Procedimento e dispositivo per allineare un veicolo spaziale, specialmente un satellite geostazionario, in una direzione di riferimento - Google Patents

Procedimento e dispositivo per allineare un veicolo spaziale, specialmente un satellite geostazionario, in una direzione di riferimento

Info

Publication number
IT9020889A0
IT9020889A0 IT9020889A IT2088990A IT9020889A0 IT 9020889 A0 IT9020889 A0 IT 9020889A0 IT 9020889 A IT9020889 A IT 9020889A IT 2088990 A IT2088990 A IT 2088990A IT 9020889 A0 IT9020889 A0 IT 9020889A0
Authority
IT
Italy
Prior art keywords
aligning
procedure
reference direction
space vehicle
geostationary satellite
Prior art date
Application number
IT9020889A
Other languages
English (en)
Other versions
IT9020889A1 (it
IT1244300B (it
Inventor
Arnold Scheit
Horst-Dieter Fischer
Original Assignee
Masserchmitt Bolkow Blohm
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 Masserchmitt Bolkow Blohm filed Critical Masserchmitt Bolkow Blohm
Publication of IT9020889A0 publication Critical patent/IT9020889A0/it
Publication of IT9020889A1 publication Critical patent/IT9020889A1/it
Application granted granted Critical
Publication of IT1244300B publication Critical patent/IT1244300B/it

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
    • 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
    • B64G1/36—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

Landscapes

  • Engineering & Computer Science (AREA)
  • Remote Sensing (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Navigation (AREA)
  • Variable-Direction Aerials And Aerial Arrays (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Radio Relay Systems (AREA)
IT02088990A 1989-07-11 1990-07-09 Procedimento e dispositivo per allineare un veicolo spaziale, specialmente un satellite geostazionario in una direzione di riferimento IT1244300B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3922761A DE3922761C2 (de) 1989-07-11 1989-07-11 Verfahren und Vorrichtung zum Ausrichten eines geostationären Satelliten in einer Referenzrichtung

Publications (3)

Publication Number Publication Date
IT9020889A0 true IT9020889A0 (it) 1990-07-09
IT9020889A1 IT9020889A1 (it) 1992-01-09
IT1244300B IT1244300B (it) 1994-07-08

Family

ID=6384728

Family Applications (1)

Application Number Title Priority Date Filing Date
IT02088990A IT1244300B (it) 1989-07-11 1990-07-09 Procedimento e dispositivo per allineare un veicolo spaziale, specialmente un satellite geostazionario in una direzione di riferimento

Country Status (5)

Country Link
US (1) US5132910A (it)
JP (1) JP2664797B2 (it)
DE (1) DE3922761C2 (it)
FR (1) FR2649809B1 (it)
IT (1) IT1244300B (it)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE69109266T2 (de) * 1990-08-22 1995-08-24 Microcosm Inc Vorrichtung zum halten eines satelliten auf seiner umlaufbahn.
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
DE4135034C2 (de) * 1991-10-23 1995-04-13 Deutsche Forsch Luft Raumfahrt Einrichtung zur Bahnkontrolle von mindestens zwei kopositionierten geostationären Satelliten
US5311435A (en) * 1991-11-27 1994-05-10 Hughes Aircraft Company Method for station keeping control of flexible spacecraft using onboard gain scheduling scheme
US5255879A (en) * 1991-11-27 1993-10-26 Hughes Aircraft Company Three axes stabilized spacecraft and method of sun acquisition
US5687084A (en) * 1992-05-26 1997-11-11 Microcosm, Inc. Satellite orbit maintenance system
US5348255A (en) * 1992-06-02 1994-09-20 Hughes Aircraft Company System and method for sensing attitude of a spacecraft with equilized star tracker errors along three orthogonal axes
FR2699701B1 (fr) * 1992-12-17 1995-03-24 Aerospatiale Procédé de contrôle d'attitude d'un satellite pointé vers un objet céleste et satellite adapté à sa mise en Óoeuvre.
US5597142A (en) * 1995-03-06 1997-01-28 Space Systems/Loral, Inc. Spacecraft acquisition of orientation by scan of earth sensor field of view
DE19510371C1 (de) * 1995-03-22 1996-10-31 Daimler Benz Aerospace Ag Verfahren zur Sonnensuche für einen dreiachsenstabilisierten Satelliten und dreiachsenstabilisierter Satellit
US5738309A (en) * 1996-02-28 1998-04-14 Hughes Electronics Single axis correction for orbit inclination
GB2318888A (en) * 1996-10-30 1998-05-06 Motorola Inc Solar panel mounted sun sensor and three-axis attitude control
JPH10170302A (ja) * 1996-12-10 1998-06-26 Toshiba Corp 方向検出装置
US6076774A (en) * 1998-08-12 2000-06-20 Hughes Electronics Corporation Fuel and thermal optimal spiral earth acquisition
US6152403A (en) * 1998-11-11 2000-11-28 Hughes Electronics Corporation Gyroscopic calibration methods for spacecraft
US6561462B1 (en) * 2002-02-21 2003-05-13 The Boeing Company Spacecraft power/sun aquistion algorithm using slit sun sensors
US6571156B1 (en) * 2002-04-01 2003-05-27 The Boeing Company Spacecraft power acquisition procedure and method for wing-deployed configuration
KR101782259B1 (ko) * 2016-04-21 2017-09-27 한국항공우주연구원 위성 안테나 속도 제어 장치 및 방법

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4325124A (en) * 1979-02-28 1982-04-13 Organisation Europeenne De Recherches Spatiales System for controlling the direction of the momentum vector of a geosynchronous satellite
US4521855A (en) * 1981-07-27 1985-06-04 Ford Aerospace & Communications Corporation Electronic on-orbit roll/yaw satellite control
US4489383A (en) * 1981-10-16 1984-12-18 Rca Corporation Closed-loop magnetic roll/yaw control system for high inclination orbit satellites
DE3214384A1 (de) * 1982-04-20 1983-10-27 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verfahren zum beibehalten der sonnenorientierung eines satelliten
US4617634A (en) * 1983-06-28 1986-10-14 Mitsubishi Denki Kabushiki Kaisha Artificial satellite attitude control system
DE3606636C1 (de) * 1986-02-28 1987-11-05 Messerschmitt Boelkow Blohm Verfahren zur Bestimmung von Erdmagnetfeldkomponenten bezueglich eines satellitenfesten Koordinatensystems
DE3607931A1 (de) * 1986-03-11 1987-09-17 Siemens Ag Fernmeldesatellitensystem auf quasistationaeren bahnen
US4827422A (en) * 1986-12-04 1989-05-02 Barnes Engineering Company Fan scan horizon sensor for a spin stabilized satellite
GB8809247D0 (en) * 1988-04-20 1988-05-25 British Aerospace Attitude recovery for spacecraft

Also Published As

Publication number Publication date
FR2649809A1 (fr) 1991-01-18
JP2664797B2 (ja) 1997-10-22
IT9020889A1 (it) 1992-01-09
US5132910A (en) 1992-07-21
JPH03217398A (ja) 1991-09-25
DE3922761C2 (de) 1994-08-25
IT1244300B (it) 1994-07-08
DE3922761A1 (de) 1991-05-02
FR2649809B1 (fr) 1994-03-18

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Legal Events

Date Code Title Description
0001 Granted
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19970729