DE69018110D1 - Gegenrotationsmechanisches Stabilisierungssystem mit eingefügten Rotoren. - Google Patents
Gegenrotationsmechanisches Stabilisierungssystem mit eingefügten Rotoren.Info
- Publication number
- DE69018110D1 DE69018110D1 DE69018110T DE69018110T DE69018110D1 DE 69018110 D1 DE69018110 D1 DE 69018110D1 DE 69018110 T DE69018110 T DE 69018110T DE 69018110 T DE69018110 T DE 69018110T DE 69018110 D1 DE69018110 D1 DE 69018110D1
- Authority
- DE
- Germany
- Prior art keywords
- rotors
- counter
- stabilization system
- mechanical stabilization
- rotation mechanical
- 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 - Fee Related
Links
- 230000006641 stabilisation Effects 0.000 title 1
- 238000011105 stabilization Methods 0.000 title 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
- B64G1/28—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect
- B64G1/283—Guiding or controlling apparatus, e.g. for attitude control using inertia or gyro effect using reaction wheels
-
- 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
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8901216A FR2642538B1 (fr) | 1989-01-31 | 1989-01-31 | Systeme de stabilisation mecanique a contre-rotation a rotors emboites |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69018110D1 true DE69018110D1 (de) | 1995-05-04 |
DE69018110T2 DE69018110T2 (de) | 1995-08-10 |
Family
ID=9378315
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE69018110T Expired - Fee Related DE69018110T2 (de) | 1989-01-31 | 1990-01-30 | Gegenrotationsmechanisches Stabilisierungssystem mit eingefügten Rotoren. |
Country Status (6)
Country | Link |
---|---|
US (1) | US5012170A (de) |
EP (1) | EP0381574B1 (de) |
CA (1) | CA2008307A1 (de) |
DE (1) | DE69018110T2 (de) |
ES (1) | ES2072995T3 (de) |
FR (1) | FR2642538B1 (de) |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5107192A (en) * | 1990-12-26 | 1992-04-21 | Sundstrand Corporation | Magnetic bearing control at critical shaft speeds |
US5357180A (en) * | 1992-08-12 | 1994-10-18 | Speicher Marcus E | Composite rotating machine |
FR2711290B1 (fr) * | 1993-10-15 | 1995-12-15 | Thomson Csf | Ensemble de radiodiffusion comportant une antenne rotative à dipôles filaires et joint rotatif conçu pour cet ensemble. |
FR2711289B1 (fr) * | 1993-10-15 | 1995-12-15 | Thomson Csf | Ensemble de radiodiffusion comportant une antenne rotative à dipôles rigides et joint rotatif conçu pour cet ensemble. |
SE505599C2 (sv) * | 1995-05-09 | 1997-09-22 | Celsiustech Electronics Ab | Antennanordning |
FR2746366B1 (fr) * | 1996-03-22 | 1998-08-14 | Aerospatiale | Procede et dispositif pour la manoeuvre rapide d'une charge utile embarquee sur une plate-forme spatiale |
US5751078A (en) * | 1996-10-03 | 1998-05-12 | Lockheed Martin Corp. Missiles & Space | Reactionless, momentum compensated payload positioner |
US6107770A (en) * | 1998-01-27 | 2000-08-22 | Lockheed Martin Corporation | Control system for counter-oscillating masses |
GB0002375D0 (en) * | 2000-02-03 | 2000-03-22 | Renishaw Plc | Reactionless rotary drive mechanism |
US6445353B1 (en) * | 2000-10-30 | 2002-09-03 | Weinbrenner, Inc. | Remote controlled actuator and antenna adjustment actuator and electronic control and digital power converter |
GB0130021D0 (en) * | 2001-12-15 | 2002-02-06 | Renishaw Plc | Reaction balanced rotary drive mechanism |
TW201105525A (en) * | 2009-08-10 | 2011-02-16 | Clearwater Holdings Ltd | Vehicle propulsion using kinetic energy transfer |
US10197792B2 (en) | 2016-02-22 | 2019-02-05 | Raytheon Company | Reaction compensated steerable platform |
US10139617B2 (en) * | 2016-02-22 | 2018-11-27 | Raytheon Company | Reaction compensated steerable platform |
Family Cites Families (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2966811A (en) * | 1959-06-01 | 1961-01-03 | Edward V Sundt | Rotator mechanism for antennas or the like |
US3514778A (en) * | 1965-10-29 | 1970-05-26 | Us Navy | Drive system for scanning antenna |
US4181283A (en) * | 1978-02-21 | 1980-01-01 | TRW Inc. Systems & Energy | Rotary mount characterized by variable coning motion |
US4158845A (en) * | 1978-03-31 | 1979-06-19 | The Boeing Company | Non-gimbaled pointer and tracking platform assembly |
US4227347A (en) * | 1978-09-14 | 1980-10-14 | Silicon Valley Group, Inc. | Two motor drive for a wafer processing machine |
US4392137A (en) * | 1980-12-22 | 1983-07-05 | Western Marine Electronics, Inc. | Radar system |
US4375047A (en) * | 1981-07-23 | 1983-02-22 | General Signal Corporation | Torque compensated electrical motor |
US4373147A (en) * | 1981-07-23 | 1983-02-08 | General Signal Corporation | Torque compensated electric motor |
FR2581257B1 (fr) * | 1982-06-08 | 1988-05-13 | Thomson Csf | Antenne a balayage conique et utilisation d'une telle antenne dans un radar de poursuite |
US4465951A (en) * | 1983-03-21 | 1984-08-14 | Satellite Business Systems | Backup bearing and power transfer assembly for communication satellite |
US4571528A (en) * | 1983-06-21 | 1986-02-18 | Magna Motive Industries, Inc. | Electromagnetic rotary motor |
JPS6011746A (ja) * | 1983-06-30 | 1985-01-22 | Toshiba Corp | フライホイ−ル装置 |
WO1986000863A1 (en) * | 1984-07-20 | 1986-02-13 | Hughes Aircraft Company | Spin-stabilized satellite with nutation control subsystem |
US4772892A (en) * | 1984-11-13 | 1988-09-20 | Raytheon Company | Two-axis gimbal |
CN1006265B (zh) * | 1985-04-01 | 1989-12-27 | 陶凤白 | 一种用于无级变速的交流电动机 |
US4752884A (en) * | 1985-07-18 | 1988-06-21 | Hughes Aircraft Company | Precision platform pointing controller for a dual-spin spacecraft |
US4761588A (en) * | 1986-12-05 | 1988-08-02 | Mit | Dual-drive system for micro-manipulation of direct-drive robotic systems |
US4824052A (en) * | 1987-06-18 | 1989-04-25 | Hughes Aircraft Company | Nutation sensor and nutation control system for a dual-spin stabilized satellite |
-
1989
- 1989-01-31 FR FR8901216A patent/FR2642538B1/fr not_active Expired - Lifetime
-
1990
- 1990-01-23 CA CA002008307A patent/CA2008307A1/en not_active Abandoned
- 1990-01-26 US US07/470,826 patent/US5012170A/en not_active Expired - Fee Related
- 1990-01-30 ES ES90400249T patent/ES2072995T3/es not_active Expired - Lifetime
- 1990-01-30 DE DE69018110T patent/DE69018110T2/de not_active Expired - Fee Related
- 1990-01-30 EP EP90400249A patent/EP0381574B1/de not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
US5012170A (en) | 1991-04-30 |
EP0381574A1 (de) | 1990-08-08 |
ES2072995T3 (es) | 1995-08-01 |
FR2642538A1 (fr) | 1990-08-03 |
FR2642538B1 (fr) | 1991-05-24 |
DE69018110T2 (de) | 1995-08-10 |
CA2008307A1 (en) | 1990-07-31 |
EP0381574B1 (de) | 1995-03-29 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
8364 | No opposition during term of opposition | ||
8339 | Ceased/non-payment of the annual fee |