FR2447320A1 - Perfectionnements aux procedes et dispositifs d'amortissement actif de nutation pour vehicule spatial - Google Patents
Perfectionnements aux procedes et dispositifs d'amortissement actif de nutation pour vehicule spatialInfo
- Publication number
- FR2447320A1 FR2447320A1 FR7901663A FR7901663A FR2447320A1 FR 2447320 A1 FR2447320 A1 FR 2447320A1 FR 7901663 A FR7901663 A FR 7901663A FR 7901663 A FR7901663 A FR 7901663A FR 2447320 A1 FR2447320 A1 FR 2447320A1
- Authority
- FR
- France
- Prior art keywords
- vehicle
- pulse
- amplitude
- devices
- nutation
- 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
Links
- 238000013016 damping Methods 0.000 title abstract 2
- 238000000034 method Methods 0.000 title 1
- 238000012986 modification Methods 0.000 abstract 1
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
- B64G1/38—Guiding or controlling apparatus, e.g. for attitude control damping of oscillations, e.g. nutation dampers
-
- 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
Abstract
AMORTISSEMENT ACTIF DES MOUVEMENTS DE NUTATION D'UN VEHICULE SPATIAL ANIME D'UN MOUVEMENT DE ROTATION AUTOUR D'UN AXE GEOMETRIQUE. ON DETECTE L'AMPLITUDE ET LA PHASE DU MOUVEMENT DE NUTATION ET ON EFFECTUE UN ECHANGE D'ENERGIE PAR IMPULSIONS ENTRE LE VEHICULE ET SON ENVIRONNEMENT LORSQUE L'AMPLITUDE DEPASSE UN SEUIL DETERMINE. ON MEMORISE LES MODIFICATIONS DU MOMENT CINETIQUE DU VEHICULE PROVOQUEES PAR LES IMPULSIONS SUCCESSIVES ET ON COMMANDE UNE IMPULSION LORSQUE L'AMPLITUDE EST SUPERIEURE AU SEUIL ET LA PHASE CORRESPOND A L'EFFICACITE MAXIMUM DE L'IMPULSION. ON INHIBE L'ORDRECHAQUE FOIS QUE L'IMPULSION TEND A AUGMENTER L'ECART DE POSITION ENTRE LE MOMENT CINETIQUE REEL ET LE MOMENT INITIAL. APPLICATIONS COURANTES.
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7901663A FR2447320A1 (fr) | 1979-01-23 | 1979-01-23 | Perfectionnements aux procedes et dispositifs d'amortissement actif de nutation pour vehicule spatial |
GB8001490A GB2040513B (en) | 1979-01-23 | 1980-01-16 | Active nutation control system for space vehicle |
US06/114,197 US4370716A (en) | 1979-01-23 | 1980-01-22 | Active nutation control system for space vehicle |
DE19803002349 DE3002349A1 (de) | 1979-01-23 | 1980-01-23 | Verfahren und vorrichtung zur daempfung der nutation eines raumfahrzeuges |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR7901663A FR2447320A1 (fr) | 1979-01-23 | 1979-01-23 | Perfectionnements aux procedes et dispositifs d'amortissement actif de nutation pour vehicule spatial |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2447320A1 true FR2447320A1 (fr) | 1980-08-22 |
FR2447320B1 FR2447320B1 (fr) | 1983-03-18 |
Family
ID=9221091
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR7901663A Granted FR2447320A1 (fr) | 1979-01-23 | 1979-01-23 | Perfectionnements aux procedes et dispositifs d'amortissement actif de nutation pour vehicule spatial |
Country Status (4)
Country | Link |
---|---|
US (1) | US4370716A (fr) |
DE (1) | DE3002349A1 (fr) |
FR (1) | FR2447320A1 (fr) |
GB (1) | GB2040513B (fr) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2581966A1 (fr) * | 1985-05-17 | 1986-11-21 | Rca Corp | Procede et systeme de stabilisation d'un vehicule spatial |
CN109573105A (zh) * | 2018-11-19 | 2019-04-05 | 上海埃依斯航天科技有限公司 | 末子级留轨应用子系统姿态控制方法 |
Families Citing this family (30)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4470568A (en) * | 1975-02-19 | 1984-09-11 | Hughes Aircraft Company | Method for changing the spin rate of a spinning body |
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 |
US4504032A (en) * | 1982-03-10 | 1985-03-12 | Rca Corporation | Control of nutation in a spacecraft |
DE3212574A1 (de) * | 1982-04-03 | 1983-10-20 | Dornier System Gmbh, 7990 Friedrichshafen | Verfahren zur lageaenderung eines satelliten |
JPS58177799A (ja) * | 1982-04-09 | 1983-10-18 | 日本電気株式会社 | 人工衛星ニユ−テ−シヨン減衰装置 |
DE3482789D1 (de) * | 1983-03-12 | 1990-08-30 | British Aerospace | Nutations-daempfung. |
US4560120A (en) * | 1983-08-19 | 1985-12-24 | The United States Of America As Represented By The Secretary Of The Army | Spin stabilized impulsively controlled missile (SSICM) |
US4728062A (en) * | 1985-11-12 | 1988-03-01 | Rca Corporation | Pivot actuated nutation damping for a dual-spin spacecraft |
US4725024A (en) * | 1985-11-15 | 1988-02-16 | Ford Aerospace & Communications Corporation | Method for spinning up a three-axis controlled spacecraft |
US4676456A (en) * | 1985-11-27 | 1987-06-30 | Raytheon Company | Strap down roll reference |
GB8616385D0 (en) * | 1986-07-04 | 1986-08-13 | Marconi Space Systems Ltd | Satellite attitude control |
US4791573A (en) * | 1986-09-02 | 1988-12-13 | Sanders Associates, Inc. | State-deviation-estimation circuit employing a phase-locked-loop phase reference |
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 |
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 |
US5098041A (en) * | 1990-06-07 | 1992-03-24 | Hughes Aircraft Company | Attitude control system for momentum-biased spacecraft |
US5163640A (en) * | 1990-12-14 | 1992-11-17 | Hughes Aircraft Company | Active spin axis control for spinning space vehicles |
US5222023A (en) * | 1991-04-02 | 1993-06-22 | Space Systems/Loral, Inc. | Compensated transition for spacecraft attitude control |
DE4129628A1 (de) * | 1991-09-06 | 1993-03-18 | Deutsche Aerospace | Verfahren und vorrichtung zur lageregelung eines dreiachsenstabilisierten, drallbehafteten raumfahrzeuges |
US5456429A (en) * | 1993-08-02 | 1995-10-10 | Loral Corp. | Thrust maneuver system |
FR2714357B1 (fr) * | 1993-12-27 | 1996-03-22 | Aerospatiale | Procédé de minimisation, amortissement ou compensation des perturbations sur un satellite stabilisé par autorotation. |
US5379968A (en) * | 1993-12-29 | 1995-01-10 | Raytheon Company | Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same |
US5425514A (en) * | 1993-12-29 | 1995-06-20 | Raytheon Company | Modular aerodynamic gyrodynamic intelligent controlled projectile and method of operating same |
US5816538A (en) * | 1994-10-13 | 1998-10-06 | Hughes Electronics Corporation | Dynamic decoupler for improved attitude control |
US5884869A (en) * | 1996-03-18 | 1999-03-23 | Hughes Electronics Corporation | Satellite spin vector control with sun sensor |
FR2846081B1 (fr) * | 2002-10-17 | 2005-01-07 | Saint Louis Inst | Pilotage d'un projectile par decharge plasma |
IL162027A (en) * | 2004-05-17 | 2009-05-04 | Rafael Advanced Defense Sys | Method and system for resetting the flight path of a non-guided bullet, including compensation for deviation from the oscillations of the launcher |
CN101275842B (zh) * | 2007-03-29 | 2010-12-15 | 北京控制工程研究所 | 中高轨道航天器的近红外光成像式自主导航敏感器系统 |
US8620496B2 (en) * | 2008-07-23 | 2013-12-31 | The Boeing Company | Systems and method of controlling a spacecraft using attitude sensors |
US8058596B2 (en) * | 2009-08-27 | 2011-11-15 | Raytheon Company | Method of controlling missile flight using attitude control thrusters |
Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1372563A (fr) * | 1963-07-31 | 1964-09-18 | Nord Aviation | Procédé pour stabiliser un solide en rotation, et dispositif correspondant |
FR1468913A (fr) * | 1965-11-13 | 1967-02-10 | Nord Aviation | Procédé et dispositif pour stabiliser, selon une direction fixe, un véhicule en rotation lente |
FR2259389A1 (fr) * | 1974-01-25 | 1975-08-22 | Hughes Aircraft Co | |
US3944172A (en) * | 1972-04-14 | 1976-03-16 | Erno Raumfahrttechnik Gmbh | Attitude control for space vehicle |
FR2373823A1 (fr) * | 1976-12-10 | 1978-07-07 | Matra | Procede et dispositif de commande d'attitude de vehicule spatial |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3558078A (en) * | 1967-08-21 | 1971-01-26 | Whittaker Corp | Space vehicle attitude control |
US3643897A (en) * | 1968-10-18 | 1972-02-22 | Communications Satellite Corp | Nutation correction system for spin-stabilized satellite |
US3624367A (en) * | 1968-11-12 | 1971-11-30 | Gen Electric | Self-optimized and adaptive attitude control system |
US4023752A (en) * | 1973-12-10 | 1977-05-17 | Rca Corporation | Elimination of residual spacecraft nutation due to propulsive torques |
US3984071A (en) * | 1974-08-29 | 1976-10-05 | Trw Inc. | Satellite nutation attenuation apparatus |
US4096427A (en) * | 1975-10-21 | 1978-06-20 | Hughes Aircraft Company | Nutation damping in dual-spin stabilized devices |
DE2732201C2 (de) * | 1977-07-16 | 1983-01-13 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Regler für die Lagestabilisierung eines Satelliten |
-
1979
- 1979-01-23 FR FR7901663A patent/FR2447320A1/fr active Granted
-
1980
- 1980-01-16 GB GB8001490A patent/GB2040513B/en not_active Expired
- 1980-01-22 US US06/114,197 patent/US4370716A/en not_active Expired - Lifetime
- 1980-01-23 DE DE19803002349 patent/DE3002349A1/de active Granted
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR1372563A (fr) * | 1963-07-31 | 1964-09-18 | Nord Aviation | Procédé pour stabiliser un solide en rotation, et dispositif correspondant |
FR1468913A (fr) * | 1965-11-13 | 1967-02-10 | Nord Aviation | Procédé et dispositif pour stabiliser, selon une direction fixe, un véhicule en rotation lente |
US3944172A (en) * | 1972-04-14 | 1976-03-16 | Erno Raumfahrttechnik Gmbh | Attitude control for space vehicle |
FR2259389A1 (fr) * | 1974-01-25 | 1975-08-22 | Hughes Aircraft Co | |
FR2373823A1 (fr) * | 1976-12-10 | 1978-07-07 | Matra | Procede et dispositif de commande d'attitude de vehicule spatial |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2581966A1 (fr) * | 1985-05-17 | 1986-11-21 | Rca Corp | Procede et systeme de stabilisation d'un vehicule spatial |
CN109573105A (zh) * | 2018-11-19 | 2019-04-05 | 上海埃依斯航天科技有限公司 | 末子级留轨应用子系统姿态控制方法 |
CN109573105B (zh) * | 2018-11-19 | 2022-06-14 | 上海埃依斯航天科技有限公司 | 末子级留轨应用子系统姿态控制方法 |
Also Published As
Publication number | Publication date |
---|---|
GB2040513A (en) | 1980-08-28 |
GB2040513B (en) | 1983-04-13 |
DE3002349C2 (fr) | 1990-07-12 |
DE3002349A1 (de) | 1980-07-31 |
US4370716A (en) | 1983-01-25 |
FR2447320B1 (fr) | 1983-03-18 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |