FR2815730B1 - Procede de commande d'attitude et de stabilisation d'un satellite en orbite basse, par couplage avec le champ magnetique terrestre - Google Patents

Procede de commande d'attitude et de stabilisation d'un satellite en orbite basse, par couplage avec le champ magnetique terrestre

Info

Publication number
FR2815730B1
FR2815730B1 FR0013392A FR0013392A FR2815730B1 FR 2815730 B1 FR2815730 B1 FR 2815730B1 FR 0013392 A FR0013392 A FR 0013392A FR 0013392 A FR0013392 A FR 0013392A FR 2815730 B1 FR2815730 B1 FR 2815730B1
Authority
FR
France
Prior art keywords
attitude
satellite
stabilization
coupling
controlling
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
FR0013392A
Other languages
English (en)
Other versions
FR2815730A1 (fr
Inventor
Ange Defendini
Kristen Lagadec
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 Defence and Space SAS
Original Assignee
Astrium 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 Astrium SAS filed Critical Astrium SAS
Priority to FR0013392A priority Critical patent/FR2815730B1/fr
Publication of FR2815730A1 publication Critical patent/FR2815730A1/fr
Application granted granted Critical
Publication of FR2815730B1 publication Critical patent/FR2815730B1/fr
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
    • B64G1/366—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using magnetometers
    • 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
    • B64G1/244—Spacecraft control systems
    • B64G1/245—Attitude control algorithms for spacecraft 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
    • B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
    • B64G1/281—Spin-stabilised spacecraft
    • 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
    • B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
FR0013392A 2000-10-19 2000-10-19 Procede de commande d'attitude et de stabilisation d'un satellite en orbite basse, par couplage avec le champ magnetique terrestre Expired - Lifetime FR2815730B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0013392A FR2815730B1 (fr) 2000-10-19 2000-10-19 Procede de commande d'attitude et de stabilisation d'un satellite en orbite basse, par couplage avec le champ magnetique terrestre

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0013392A FR2815730B1 (fr) 2000-10-19 2000-10-19 Procede de commande d'attitude et de stabilisation d'un satellite en orbite basse, par couplage avec le champ magnetique terrestre

Publications (2)

Publication Number Publication Date
FR2815730A1 FR2815730A1 (fr) 2002-04-26
FR2815730B1 true FR2815730B1 (fr) 2003-10-24

Family

ID=8855509

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0013392A Expired - Lifetime FR2815730B1 (fr) 2000-10-19 2000-10-19 Procede de commande d'attitude et de stabilisation d'un satellite en orbite basse, par couplage avec le champ magnetique terrestre

Country Status (1)

Country Link
FR (1) FR2815730B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103991559B (zh) * 2014-05-28 2016-02-17 中国人民解放军国防科学技术大学 一种洛伦兹航天器悬停控制方法
CN109649693B (zh) * 2019-01-21 2021-12-14 上海微小卫星工程中心 一种纯磁控自旋对日定向方法
CN111060111A (zh) * 2019-12-23 2020-04-24 北京国电高科科技有限公司 一种低轨卫星入轨初期定轨方法

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2630398B1 (fr) * 1988-04-26 1990-08-24 Aerospatiale Procede de basculement du moment d'inertie d'un corps rotatif libre dans l'espace jusqu'en une direction donnee
FR2742243B1 (fr) * 1995-12-06 1998-02-13 Matra Marconi Space France Procede de commande d'attitude d'un satellite en orbite basse, a acquisition solaire

Also Published As

Publication number Publication date
FR2815730A1 (fr) 2002-04-26

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