FR3010806B1 - METHOD FOR DETERMINING A PROFILE OF ATTITUDES OF A SATELLITE; COMPUTER PROGRAM PRODUCT - Google Patents

METHOD FOR DETERMINING A PROFILE OF ATTITUDES OF A SATELLITE; COMPUTER PROGRAM PRODUCT

Info

Publication number
FR3010806B1
FR3010806B1 FR1358959A FR1358959A FR3010806B1 FR 3010806 B1 FR3010806 B1 FR 3010806B1 FR 1358959 A FR1358959 A FR 1358959A FR 1358959 A FR1358959 A FR 1358959A FR 3010806 B1 FR3010806 B1 FR 3010806B1
Authority
FR
France
Prior art keywords
attitudes
satellite
profile
determining
computer program
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.)
Active
Application number
FR1358959A
Other languages
French (fr)
Other versions
FR3010806A1 (en
Inventor
Antoine Flipo
Franck Darnon
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
Priority to FR1358959A priority Critical patent/FR3010806B1/en
Publication of FR3010806A1 publication Critical patent/FR3010806A1/en
Application granted granted Critical
Publication of FR3010806B1 publication Critical patent/FR3010806B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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
    • B64G1/244—Spacecraft control systems

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)
  • Photovoltaic Devices (AREA)
FR1358959A 2013-09-18 2013-09-18 METHOD FOR DETERMINING A PROFILE OF ATTITUDES OF A SATELLITE; COMPUTER PROGRAM PRODUCT Active FR3010806B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR1358959A FR3010806B1 (en) 2013-09-18 2013-09-18 METHOD FOR DETERMINING A PROFILE OF ATTITUDES OF A SATELLITE; COMPUTER PROGRAM PRODUCT

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1358959A FR3010806B1 (en) 2013-09-18 2013-09-18 METHOD FOR DETERMINING A PROFILE OF ATTITUDES OF A SATELLITE; COMPUTER PROGRAM PRODUCT

Publications (2)

Publication Number Publication Date
FR3010806A1 FR3010806A1 (en) 2015-03-20
FR3010806B1 true FR3010806B1 (en) 2016-12-09

Family

ID=50069035

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1358959A Active FR3010806B1 (en) 2013-09-18 2013-09-18 METHOD FOR DETERMINING A PROFILE OF ATTITUDES OF A SATELLITE; COMPUTER PROGRAM PRODUCT

Country Status (1)

Country Link
FR (1) FR3010806B1 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111007865B (en) * 2019-12-18 2023-07-14 中国人民解放军国防科技大学 Satellite stable earth orientation method taking earth orientation deviation as constraint
CN111483618B (en) * 2020-04-09 2021-10-01 上海航天控制技术研究所 Multi-directional driving task autonomous management control method suitable for Mars detection

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6318676B1 (en) * 2000-01-10 2001-11-20 Space Systems/Loral, Inc. Equatorial-normal body-stabilized spacecraft and control method for inclined orbit operation

Also Published As

Publication number Publication date
FR3010806A1 (en) 2015-03-20

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