CA1073988A - Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits - Google Patents
Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbitsInfo
- Publication number
- CA1073988A CA1073988A CA256,719A CA256719A CA1073988A CA 1073988 A CA1073988 A CA 1073988A CA 256719 A CA256719 A CA 256719A CA 1073988 A CA1073988 A CA 1073988A
- Authority
- CA
- Canada
- Prior art keywords
- roll
- satellite
- yaw
- axis
- magnetic
- 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
- 239000013598 vector Substances 0.000 claims description 29
- 230000008859 change Effects 0.000 claims description 2
- 230000002238 attenuated effect Effects 0.000 claims 1
- 230000003993 interaction Effects 0.000 abstract description 2
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- 238000010586 diagram Methods 0.000 description 11
- 230000000694 effects Effects 0.000 description 10
- 238000005094 computer simulation Methods 0.000 description 3
- 230000005484 gravity Effects 0.000 description 3
- 230000004044 response Effects 0.000 description 3
- 238000009987 spinning Methods 0.000 description 3
- 230000001360 synchronised effect Effects 0.000 description 3
- 238000006243 chemical reaction Methods 0.000 description 2
- 230000008878 coupling Effects 0.000 description 2
- 238000010168 coupling process Methods 0.000 description 2
- 238000005859 coupling reaction Methods 0.000 description 2
- 238000006880 cross-coupling reaction Methods 0.000 description 2
- 238000013016 damping Methods 0.000 description 2
- 230000003247 decreasing effect Effects 0.000 description 2
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- RZVAJINKPMORJF-UHFFFAOYSA-N Acetaminophen Chemical compound CC(=O)NC1=CC=C(O)C=C1 RZVAJINKPMORJF-UHFFFAOYSA-N 0.000 description 1
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- 230000007812 deficiency Effects 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000003292 diminished effect Effects 0.000 description 1
- 238000005259 measurement Methods 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
- B64G1/36—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors
- B64G1/365—Guiding or controlling apparatus, e.g. for attitude control using sensors, e.g. sun-sensors, horizon sensors using horizon or Earth sensors
-
- 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
- B64G1/32—Guiding or controlling apparatus, e.g. for attitude control using earth's magnetic field
Landscapes
- Engineering & Computer Science (AREA)
- Remote Sensing (AREA)
- Radar, Positioning & Navigation (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Life Sciences & Earth Sciences (AREA)
- Geochemistry & Mineralogy (AREA)
- Geology (AREA)
- Environmental & Geological Engineering (AREA)
- Life Sciences & Earth Sciences (AREA)
- Automation & Control Theory (AREA)
- Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB30390/75A GB1544083A (en) | 1975-07-21 | 1975-07-21 | Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits |
| US05/640,147 US4062509A (en) | 1975-07-21 | 1975-12-12 | Closed loop roll/yaw control system for satellites |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CA1073988A true CA1073988A (en) | 1980-03-18 |
Family
ID=26260420
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CA256,719A Expired CA1073988A (en) | 1975-07-21 | 1976-07-09 | Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits |
Country Status (4)
| Country | Link |
|---|---|
| JP (1) | JPS5213300A (cs) |
| CA (1) | CA1073988A (cs) |
| DE (1) | DE2632864C2 (cs) |
| FR (1) | FR2319150A1 (cs) |
Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4424948A (en) * | 1981-01-22 | 1984-01-10 | Rca Corporation | Magnetically torqued nutation damping |
| JPS5851319A (ja) * | 1981-09-24 | 1983-03-26 | Ricoh Co Ltd | 定電圧電源装置 |
| DE3214373A1 (de) * | 1982-04-20 | 1983-10-27 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Verfahren und einrichtung fuer die lageregelung eines satelliten |
Family Cites Families (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3232561A (en) * | 1963-06-06 | 1966-02-01 | Honeywell Inc | Control apparatus for space craft |
| US3429524A (en) * | 1965-07-19 | 1969-02-25 | Westinghouse Electric Corp | Attitude control system |
| FR1602955A (cs) * | 1968-06-25 | 1971-03-01 | ||
| NL6914824A (cs) * | 1968-10-01 | 1970-04-03 | ||
| JPS537720B1 (cs) * | 1970-07-29 | 1978-03-20 | ||
| US3834653A (en) * | 1972-03-27 | 1974-09-10 | Rca Corp | Closed loop roll and yaw control for satellites |
| JPS50107700A (cs) * | 1974-02-04 | 1975-08-25 |
-
1976
- 1976-07-09 CA CA256,719A patent/CA1073988A/en not_active Expired
- 1976-07-19 FR FR7621997A patent/FR2319150A1/fr active Granted
- 1976-07-21 JP JP51087715A patent/JPS5213300A/ja active Granted
- 1976-07-21 DE DE2632864A patent/DE2632864C2/de not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| DE2632864A1 (de) | 1977-02-24 |
| FR2319150A1 (fr) | 1977-02-18 |
| FR2319150B1 (cs) | 1982-11-12 |
| JPS5213300A (en) | 1977-02-01 |
| JPH0219040B2 (cs) | 1990-04-27 |
| DE2632864C2 (de) | 1982-08-12 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US4062509A (en) | Closed loop roll/yaw control system for satellites | |
| US3834653A (en) | Closed loop roll and yaw control for satellites | |
| US4084773A (en) | Magnetic control of spacecraft roll disturbance torques | |
| CA2040463C (en) | Spacecraft earth-pointing attitude acquisition method | |
| US5349532A (en) | Spacecraft attitude control and momentum unloading using gimballed and throttled thrusters | |
| US4911385A (en) | Attitude pointing error correction system and method for geosynchronous satellites | |
| US4230294A (en) | Closed loop roll control for momentum biased satellites | |
| US4489383A (en) | Closed-loop magnetic roll/yaw control system for high inclination orbit satellites | |
| US4084772A (en) | Roll/yaw body steering for momentum biased spacecraft | |
| CN113335567B (zh) | 一种微小卫星的轮磁混合姿态控制方法和系统 | |
| US3695554A (en) | Nutation damping in dual-spin spacecraft | |
| JPH04308906A (ja) | 近赤道軌道内の３軸安定衛星用の姿勢制御システム | |
| US3232561A (en) | Control apparatus for space craft | |
| US4052654A (en) | Gyro stabilized inertial reference system with gimbal lock prevention means | |
| US4424948A (en) | Magnetically torqued nutation damping | |
| US3429524A (en) | Attitude control system | |
| US4193570A (en) | Active nutation controller | |
| US4504032A (en) | Control of nutation in a spacecraft | |
| US5062583A (en) | High accuracy bank-to-turn autopilot | |
| CA1073988A (en) | Precision closed loop roll and yaw control for momentum biased satellites in low inclination orbits | |
| US4807835A (en) | Spacecraft attitude stabilization system | |
| US3648525A (en) | Gyroscopic stable reference apparatus | |
| Bowers et al. | Orbital gyrocompassing heading reference. | |
| US3310986A (en) | Three axis navigational apparatus | |
| Black et al. | An electromagnetic attitude control system for a synchronous satellite. |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MKEX | Expiry |