JPS6363440B2 - - Google Patents
Info
- Publication number
- JPS6363440B2 JPS6363440B2 JP55115787A JP11578780A JPS6363440B2 JP S6363440 B2 JPS6363440 B2 JP S6363440B2 JP 55115787 A JP55115787 A JP 55115787A JP 11578780 A JP11578780 A JP 11578780A JP S6363440 B2 JPS6363440 B2 JP S6363440B2
- Authority
- JP
- Japan
- Prior art keywords
- spacecraft
- jet
- torque
- rocket
- main axis
- 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
Links
- 235000015842 Hesperis Nutrition 0.000 claims description 36
- 235000012633 Iberis amara Nutrition 0.000 claims description 36
- 238000006243 chemical reaction Methods 0.000 claims description 8
- 230000000694 effects Effects 0.000 description 10
- 239000013598 vector Substances 0.000 description 8
- OAKJQQAXSVQMHS-UHFFFAOYSA-N Hydrazine Chemical compound NN OAKJQQAXSVQMHS-UHFFFAOYSA-N 0.000 description 6
- 238000010586 diagram Methods 0.000 description 6
- 238000000034 method Methods 0.000 description 3
- 238000004891 communication Methods 0.000 description 2
- 238000000354 decomposition reaction Methods 0.000 description 2
- 239000012530 fluid Substances 0.000 description 2
- 238000010276 construction Methods 0.000 description 1
- 230000007423 decrease Effects 0.000 description 1
- 230000003247 decreasing effect Effects 0.000 description 1
- 238000009792 diffusion process Methods 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000446 fuel Substances 0.000 description 1
- 238000002347 injection Methods 0.000 description 1
- 239000007924 injection Substances 0.000 description 1
- 239000003380 propellant Substances 0.000 description 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
- B64G1/26—Guiding or controlling apparatus, e.g. for attitude control using jets
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Radar, Positioning & Navigation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
- Steering-Linkage Mechanisms And Four-Wheel Steering (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US6850279A | 1979-08-22 | 1979-08-22 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS5634600A JPS5634600A (en) | 1981-04-06 |
| JPS6363440B2 true JPS6363440B2 (enExample) | 1988-12-07 |
Family
ID=22082995
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP11578780A Granted JPS5634600A (en) | 1979-08-22 | 1980-08-21 | Controlling system for attitude for spaceship |
Country Status (4)
| Country | Link |
|---|---|
| JP (1) | JPS5634600A (enExample) |
| DE (1) | DE3031763C2 (enExample) |
| FR (1) | FR2469346A1 (enExample) |
| GB (1) | GB2056392B (enExample) |
Families Citing this family (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2251834B (en) * | 1983-02-22 | 1992-12-16 | George Alexander Tarrant | Guided missiles |
| US5251855A (en) * | 1990-05-09 | 1993-10-12 | Agence Spatiale Europeenne | Spacecraft propulsion system thruster firing system |
| FR2661889B1 (fr) * | 1990-05-09 | 1994-09-09 | Europ Agence Spatiale | Systeme propulsif pour un engin spatial stabilise en rotation et procede de commande de sa mise a feu. |
| FR2710314B1 (fr) * | 1993-09-23 | 1995-12-15 | Aerospatiale | Satellite stabilisé 3-axes à pointage géocentrique en orbite basse à générateur solaire orientable 1-axe. |
| US5813633A (en) * | 1995-12-22 | 1998-09-29 | Hughes Electronics Corporation | Method and apparatus for stationkeeping a satellite offset by pitch rotation |
| US10464694B1 (en) * | 2017-03-23 | 2019-11-05 | Space Systems/Loral, Llc | Asymmetric thruster gimbal configuration |
| CN114264446B (zh) * | 2021-12-23 | 2023-08-29 | 中电科蓝天科技股份有限公司 | 一种多自由度位姿可调的电推进羽流试验工装 |
| CN120027038B (zh) * | 2025-04-22 | 2025-07-22 | 山东协和学院 | 一种脉冲式电磁推力器羽流特性分析系统及方法 |
Family Cites Families (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3866025A (en) * | 1972-03-17 | 1975-02-11 | Rca Corp | Spacecraft attitude control system |
| DE2642061C2 (de) * | 1976-09-18 | 1983-11-24 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Lageregelungs- und Bahnänderungsverfahren für einen dreiachsenstabilisierbaren Satelliten, insbesondere für einen geostationären Satelliten und Einrichtung zur Durchführung des Verfahrens |
-
1980
- 1980-08-15 GB GB8026787A patent/GB2056392B/en not_active Expired
- 1980-08-21 JP JP11578780A patent/JPS5634600A/ja active Granted
- 1980-08-22 DE DE3031763A patent/DE3031763C2/de not_active Expired
- 1980-08-22 FR FR8018362A patent/FR2469346A1/fr active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| DE3031763A1 (de) | 1981-03-26 |
| FR2469346A1 (fr) | 1981-05-22 |
| GB2056392B (en) | 1983-08-03 |
| FR2469346B1 (enExample) | 1984-11-30 |
| GB2056392A (en) | 1981-03-18 |
| JPS5634600A (en) | 1981-04-06 |
| DE3031763C2 (de) | 1982-06-24 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| JP3220142B2 (ja) | 太陽放射の圧力による衛星のピッチ姿勢の制御方法、および該方法を行うための衛星 | |
| US5692707A (en) | Universal spacecraft attitude steering control system | |
| US8113468B2 (en) | Precision attitude control system for gimbaled thruster | |
| EP0568209B1 (en) | Spacecraft attitude control and momentum unloading using gimballed and throttled thrusters | |
| JP3244717B2 (ja) | モーメンタムバイアス宇宙船の傾斜軌道姿勢制御を行うための方法及び装置 | |
| AU639504B2 (en) | Satellite roll and yaw attitude control method | |
| Psiaki | Nanosatellite attitude stabilization using passive aerodynamics and active magnetic torquing | |
| US5383631A (en) | Triaxially stabilized satellite provided with electric propulsors for orbital maneuvering and attitude control | |
| US6053455A (en) | Spacecraft attitude control system using low thrust thrusters | |
| US4407469A (en) | Attitude control system for spacecraft utilizing the thruster plume | |
| US6360996B1 (en) | Steering control for skewed scissors pair CMG clusters | |
| JP2021165136A (ja) | 電気スラスタを備えた地球周回衛星のための操作システム | |
| JPH0655599B2 (ja) | ３軸制御宇宙船をスピンアツプするための方法 | |
| US20210284361A1 (en) | Systems and methods for attitude control for a satellite | |
| JPS6363440B2 (enExample) | ||
| JPH115599A (ja) | 宇宙船姿勢制御装置及びその方法 | |
| Gong et al. | Passive stability design for solar sail on displaced orbits | |
| US3070330A (en) | Attitude and propellant flow control system and method | |
| Liden | A new fail operational control moment gyro configuration | |
| US12330819B2 (en) | Satellite for rendezvous using electric propulsion thrusters | |
| Kaplan | Design and Operational Aspects of All-Electric Thruster Control Systems for Geostationary Satellites | |
| LEROY et al. | Spacecraft attitude control for a solar electric geosynchronous transfer mission | |
| JP2001063700A (ja) | 人工衛星の軌道制御方法、及びビーム照射領域の制御方法、並びに人工衛星システム | |
| Leveque et al. | Trajectory simulations for thrust-vectored electric propulsion missions | |
| JPH0141560B2 (enExample) |