FR2348107A1 - Procede de regulation de la tension de bord et de pilotage d'un engin spatial - Google Patents

Procede de regulation de la tension de bord et de pilotage d'un engin spatial

Info

Publication number
FR2348107A1
FR2348107A1 FR7611087A FR7611087A FR2348107A1 FR 2348107 A1 FR2348107 A1 FR 2348107A1 FR 7611087 A FR7611087 A FR 7611087A FR 7611087 A FR7611087 A FR 7611087A FR 2348107 A1 FR2348107 A1 FR 2348107A1
Authority
FR
France
Prior art keywords
motor generators
type motor
cells
obscured
return
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.)
Granted
Application number
FR7611087A
Other languages
English (en)
Other versions
FR2348107B1 (fr
Inventor
Francis Legrand
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
Priority to FR7611087A priority Critical patent/FR2348107A1/fr
Priority to BE176679A priority patent/BE853550A/fr
Priority to GB15371/77A priority patent/GB1577148A/en
Priority to CH457177A priority patent/CH615632A5/fr
Priority to DE2716538A priority patent/DE2716538C2/de
Priority to US05/787,653 priority patent/US4164018A/en
Publication of FR2348107A1 publication Critical patent/FR2348107A1/fr
Application granted granted Critical
Publication of FR2348107B1 publication Critical patent/FR2348107B1/fr
Granted 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/44—Arrangements or adaptations of power supply systems using radiation, e.g. deployable solar arrays
    • B64G1/443—Photovoltaic cell arrays
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/425—Power storage
    • B64G1/426—Flywheels
    • 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
    • B64G1/42—Arrangements or adaptations of power supply systems
    • B64G1/428—Power distribution and management
FR7611087A 1976-04-14 1976-04-14 Procede de regulation de la tension de bord et de pilotage d'un engin spatial Granted FR2348107A1 (fr)

Priority Applications (6)

Application Number Priority Date Filing Date Title
FR7611087A FR2348107A1 (fr) 1976-04-14 1976-04-14 Procede de regulation de la tension de bord et de pilotage d'un engin spatial
BE176679A BE853550A (fr) 1976-04-14 1977-04-13 Procede de regulation de la tension de bord et de pilotage d'un engin spatial
GB15371/77A GB1577148A (en) 1976-04-14 1977-04-13 Method and inertial device for steering a spacecraft and regulating its onboard supply voltage
CH457177A CH615632A5 (fr) 1976-04-14 1977-04-13
DE2716538A DE2716538C2 (de) 1976-04-14 1977-04-14 Verfahren zur Steuerung der Lage und zur Regulierung der Bordspannung eines Raumfahrzeuges sowie Trägheitsanordnung zur Durchführung eines solchen Verfahrens
US05/787,653 US4164018A (en) 1976-04-14 1977-04-14 Method and apparatus for steering a spacecraft and regulating its onboard supply voltage

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR7611087A FR2348107A1 (fr) 1976-04-14 1976-04-14 Procede de regulation de la tension de bord et de pilotage d'un engin spatial

Publications (2)

Publication Number Publication Date
FR2348107A1 true FR2348107A1 (fr) 1977-11-10
FR2348107B1 FR2348107B1 (fr) 1979-05-11

Family

ID=9171858

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7611087A Granted FR2348107A1 (fr) 1976-04-14 1976-04-14 Procede de regulation de la tension de bord et de pilotage d'un engin spatial

Country Status (2)

Country Link
BE (1) BE853550A (fr)
FR (1) FR2348107A1 (fr)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2823910A1 (de) * 1977-05-31 1978-12-21 Aerospatiale Verfahren und integrierte vorrichtung zur steuerung des drehmoments und zur einstellung der energieversorgung fuer einen raumflugkoerper
FR2423808A1 (fr) * 1978-04-18 1979-11-16 Matra Perfectionnements aux procedes et dispositifs de commande d'attitude et de stockage d'energie pour vehicule spatial
FR2489247A1 (en) * 1980-08-29 1982-03-05 Messerschmitt Boelkow Blohm Controller for satellite orientation during earth's shadow transition - uses selected revolution rate delay of on-board gyroscope

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2823910A1 (de) * 1977-05-31 1978-12-21 Aerospatiale Verfahren und integrierte vorrichtung zur steuerung des drehmoments und zur einstellung der energieversorgung fuer einen raumflugkoerper
FR2423808A1 (fr) * 1978-04-18 1979-11-16 Matra Perfectionnements aux procedes et dispositifs de commande d'attitude et de stockage d'energie pour vehicule spatial
FR2489247A1 (en) * 1980-08-29 1982-03-05 Messerschmitt Boelkow Blohm Controller for satellite orientation during earth's shadow transition - uses selected revolution rate delay of on-board gyroscope

Also Published As

Publication number Publication date
BE853550A (fr) 1977-10-13
FR2348107B1 (fr) 1979-05-11

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Legal Events

Date Code Title Description
ST Notification of lapse