FIELD: electrical mechanical executive devices of orientation of the artificial Earth satellites on the bases of paired gyroscopes.
SUBSTANCE: the arrangement has two gyroscopes with kinematics connected gimbal suspensions provided with electric drives of turning. At that gimbal suspensions with electrical drives of turning are located inside the rotors of the gyroscopes.
EFFECT: decreases weight and dimensions.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| POWER GYROSCOPIC ARRANGEMENT FOR COSMIC APPARATUS'S ORIENTATION | 1973 |
|
SU1839792A1 |
| METHOD OF DETERMINATION OF ERROR OF ELECTROSTATIC GYROSCOPE | 2001 |
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RU2193162C1 |
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|
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|
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| MOTION-PICTURE CAMERA THREE-AXIS GYRO STABILIZER | 0 |
|
SU979855A1 |
| GYROSCOPIC STABILIZER | 1986 |
|
SU1839920A1 |
