FR2022287A1 - - Google Patents

Info

Publication number
FR2022287A1
FR2022287A1 FR6935687A FR6935687A FR2022287A1 FR 2022287 A1 FR2022287 A1 FR 2022287A1 FR 6935687 A FR6935687 A FR 6935687A FR 6935687 A FR6935687 A FR 6935687A FR 2022287 A1 FR2022287 A1 FR 2022287A1
Authority
FR
France
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.)
Withdrawn
Application number
FR6935687A
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.)
NAL ETU SPATIALES CENTRE
Original Assignee
NAL ETU SPATIALES CENTRE
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 NAL ETU SPATIALES CENTRE filed Critical NAL ETU SPATIALES CENTRE
Publication of FR2022287A1 publication Critical patent/FR2022287A1/fr
Withdrawn legal-status Critical Current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
    • B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
    • 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
    • B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
FR6935687A 1968-10-18 1969-10-17 Withdrawn FR2022287A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US76863168A 1968-10-18 1968-10-18

Publications (1)

Publication Number Publication Date
FR2022287A1 true FR2022287A1 (fr) 1970-07-31

Family

ID=25083039

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6935687A Withdrawn FR2022287A1 (fr) 1968-10-18 1969-10-17

Country Status (4)

Country Link
US (1) US3643897A (fr)
DE (1) DE1943861C3 (fr)
FR (1) FR2022287A1 (fr)
GB (1) GB1286087A (fr)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3907226A (en) * 1970-07-06 1975-09-23 Hughes Aircraft Co Redundant position and attitude control for spin stabilized devices
US3811641A (en) * 1971-06-18 1974-05-21 Martin Marietta Corp Precession control device for a class of spin stabilized space vehicles
US3944172A (en) * 1972-04-14 1976-03-16 Erno Raumfahrttechnik Gmbh Attitude control for space vehicle
US3997137A (en) * 1973-12-10 1976-12-14 Rca Corporation Minimization of residual spacecraft nutation due to disturbing torques
US3937423A (en) * 1974-01-25 1976-02-10 Hughes Aircraft Company Nutation and roll error angle correction means
US3984071A (en) * 1974-08-29 1976-10-05 Trw Inc. Satellite nutation attenuation apparatus
DE2732201C2 (de) * 1977-07-16 1983-01-13 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Regler für die Lagestabilisierung eines Satelliten
US4193570A (en) * 1978-04-19 1980-03-18 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Active nutation controller
USRE30429E (en) * 1978-12-12 1980-11-04 Rca Corporation Minimization of residual spacecraft nutation due to disturbing torques
FR2447320A1 (fr) * 1979-01-23 1980-08-22 Matra Perfectionnements aux procedes et dispositifs d'amortissement actif de nutation pour vehicule spatial
JPS55164600A (en) * 1979-06-07 1980-12-22 Nippon Electric Co Nutation controller for artificial satellite
US4386750A (en) * 1980-08-29 1983-06-07 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Method of damping nutation motion with minimum spin axis attitude disturbance
DE3212574A1 (de) * 1982-04-03 1983-10-20 Dornier System Gmbh, 7990 Friedrichshafen Verfahren zur lageaenderung eines satelliten
US4599697A (en) * 1982-08-11 1986-07-08 Ford Aerospace & Communications Corporation Digital PWPF three axis spacecraft attitude control
US4537375A (en) * 1983-04-21 1985-08-27 Ford Aerospace & Communications Corporation Method and apparatus for thruster transient control
US4630790A (en) * 1984-11-19 1986-12-23 Ford Aerospace & Communications Corporation Velocity and attitude control for exoatmospheric projectile
US4730798A (en) * 1985-03-08 1988-03-15 Wertz James R Autonomous spacecraft controller and related method
JP2518212B2 (ja) * 1986-06-26 1996-07-24 日本電気株式会社 人工衛星の軌道制御方式
US4848706A (en) * 1988-02-29 1989-07-18 Ford Aerospace Corporation Spacecraft attitude control using coupled thrusters
US4931942A (en) * 1988-05-26 1990-06-05 Ford Aerospace Corporation Transition control system for spacecraft attitude control
US4916622A (en) * 1988-06-16 1990-04-10 General Electric Company Attitude control system
US5222023A (en) * 1991-04-02 1993-06-22 Space Systems/Loral, Inc. Compensated transition for spacecraft attitude control
DE4320758C2 (de) * 1993-06-23 1995-06-29 Assidomaen Packmaster Gmbh Verpackungsmaterialzuschnitt sowie ein Verfahren und eine Vorrichtung zum Verpacken einer Mehrzahl von Behältnissen, insbesondere Flaschen
US5456429A (en) * 1993-08-02 1995-10-10 Loral Corp. Thrust maneuver system
US8058596B2 (en) * 2009-08-27 2011-11-15 Raytheon Company Method of controlling missile flight using attitude control thrusters
US9518807B2 (en) * 2014-07-16 2016-12-13 Rosemount Aerospace Inc. Projectile control systems and methods
CN105253330B (zh) * 2015-10-30 2017-04-05 中国空间技术研究院 一种基于优化的信息融合geo卫星控制系统菜单式设计方法

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3189299A (en) * 1963-08-27 1965-06-15 Howell D Garner Dynamic precession damper for spin stabilized vehicles
US3362229A (en) * 1964-01-23 1968-01-09 Gen Motors Corp Transverse angular velocity sensor
US3365147A (en) * 1965-04-12 1968-01-23 Honeywell Inc Control apparatus for steerable craft
US3384323A (en) * 1965-09-27 1968-05-21 Ltv Aerospace Corp Attitude and coning control system for spin-stabilized vehicles
US3414214A (en) * 1966-05-31 1968-12-03 Trw Inc Satellite positioning system

Also Published As

Publication number Publication date
DE1943861B2 (de) 1980-11-13
DE1943861A1 (de) 1970-08-20
DE1943861C3 (de) 1981-07-23
US3643897A (en) 1972-02-22
GB1286087A (en) 1972-08-16

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Legal Events

Date Code Title Description
ST Notification of lapse