FR3033056B1 - METHOD FOR DETERMINING THE GUIDANCE PARAMETERS OF A SATELLITE FOR FOLLOWING A TRACK - Google Patents

METHOD FOR DETERMINING THE GUIDANCE PARAMETERS OF A SATELLITE FOR FOLLOWING A TRACK Download PDF

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Publication number
FR3033056B1
FR3033056B1 FR1551617A FR1551617A FR3033056B1 FR 3033056 B1 FR3033056 B1 FR 3033056B1 FR 1551617 A FR1551617 A FR 1551617A FR 1551617 A FR1551617 A FR 1551617A FR 3033056 B1 FR3033056 B1 FR 3033056B1
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France
Prior art keywords
satellite
determining
trajectory
point
following
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
FR1551617A
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French (fr)
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FR3033056A1 (en
Inventor
Nicolas Theret
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
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Centre National dEtudes Spatiales CNES
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Publication date
Application filed by Centre National dEtudes Spatiales CNES filed Critical Centre National dEtudes Spatiales CNES
Priority to FR1551617A priority Critical patent/FR3033056B1/en
Priority to PCT/EP2016/053781 priority patent/WO2016135144A1/en
Publication of FR3033056A1 publication Critical patent/FR3033056A1/en
Application granted granted Critical
Publication of FR3033056B1 publication Critical patent/FR3033056B1/en
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Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/242Orbits and trajectories
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/10Artificial satellites; Systems of such satellites; Interplanetary vehicles
    • B64G1/1021Earth observation satellites
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64GCOSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
    • B64G1/00Cosmonautic vehicles
    • B64G1/22Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
    • B64G1/24Guiding or controlling apparatus, e.g. for attitude control
    • B64G1/244Spacecraft control systems

Landscapes

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

Abstract

L'invention concerne un procédé de détermination des paramètres de guidage d'un satellite pour suivre une trajectoire comprenant au moins deux cibles pour lesquelles le satellite doit effectuer une acquisition, le procédé comprenant des étapes de - détermination d'une trajectoire passant par lesdites cibles ; - détermination des paramètres de guidage pour passer à un point de la trajectoire comprenant des sous-étapes de - détermination d'une direction à suivre au point de la trajectoire, ladite direction à suivre étant tangente à la trajectoire audit point considéré ; - détermination, à partir de ladite direction à suivre au point considéré, des paramètres de guidage du satellite pour passer par ledit point considéré selon une direction du satellite alignée avec la direction à suivre.The invention relates to a method for determining the guidance parameters of a satellite for following a trajectory comprising at least two targets for which the satellite must make an acquisition, the method comprising steps for determining a trajectory passing through said targets. ; determination of the guiding parameters for passing to a point of the trajectory comprising substeps of determining a direction to follow at the point of the trajectory, said direction to follow being tangent to the trajectory at said point considered; determination, from said direction to be followed at the point in question, of the satellite guidance parameters for passing through said considered point in a direction of the satellite aligned with the direction to be followed.

FR1551617A 2015-02-25 2015-02-25 METHOD FOR DETERMINING THE GUIDANCE PARAMETERS OF A SATELLITE FOR FOLLOWING A TRACK Active FR3033056B1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR1551617A FR3033056B1 (en) 2015-02-25 2015-02-25 METHOD FOR DETERMINING THE GUIDANCE PARAMETERS OF A SATELLITE FOR FOLLOWING A TRACK
PCT/EP2016/053781 WO2016135144A1 (en) 2015-02-25 2016-02-23 Method for determining the guide parameters of a satellite in order to make the line of sight of the instrument thereof follow a trajectory

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR1551617 2015-02-25
FR1551617A FR3033056B1 (en) 2015-02-25 2015-02-25 METHOD FOR DETERMINING THE GUIDANCE PARAMETERS OF A SATELLITE FOR FOLLOWING A TRACK

Publications (2)

Publication Number Publication Date
FR3033056A1 FR3033056A1 (en) 2016-08-26
FR3033056B1 true FR3033056B1 (en) 2019-05-03

Family

ID=53758304

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1551617A Active FR3033056B1 (en) 2015-02-25 2015-02-25 METHOD FOR DETERMINING THE GUIDANCE PARAMETERS OF A SATELLITE FOR FOLLOWING A TRACK

Country Status (2)

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FR (1) FR3033056B1 (en)
WO (1) WO2016135144A1 (en)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111666694B (en) * 2020-06-15 2022-11-08 中国电子科技集团公司第二十八研究所 Position-balanced target group motion process simulation calculation method
CN111897357B (en) * 2020-08-13 2023-10-20 上海航天控制技术研究所 Attitude tracking control method for satellite earth scanning
CN115167498B (en) * 2022-08-23 2024-05-03 中国电子科技集团公司第三十八研究所 Method and system for updating working parameters of yaw guide low-orbit radar imaging satellite

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5100084A (en) * 1990-04-16 1992-03-31 Space Systems/Loral, Inc. Method and apparatus for inclined orbit attitude control for momentum bias spacecraft
US8386098B2 (en) * 2009-08-03 2013-02-26 David A. Bailey Method for a deeper search in a time-limited image satellite planning environment
US9126700B2 (en) * 2010-01-25 2015-09-08 Tarik Ozkul Autonomous decision system for selecting target in observation satellites

Also Published As

Publication number Publication date
WO2016135144A1 (en) 2016-09-01
FR3033056A1 (en) 2016-08-26

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