FIELD: electrical mechanical executive devices of controlling of angular position of cosmic flying apparatus fulfilled on the basis of paired gyroscopes.
SUBSTANCE: the arrangement has two-degree -of- freedom gyroscopes with mechanical synchronization of suspensions and electrical drives along these axes. At that on every mechanism of synchronization measurers of moments are installed. The exits of the measurers of moments are connected through intensive-converting blocks with inputs of controlling of electrical drives.
EFFECT: increases reliability of the work.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ARRANGEMENT FOR CONTROLLING OF COSMIC APPARATUS'S ORIENTATION | 1976 |
|
SU1839794A1 |
| POWER GYROSCOPIC ARRANGEMENT | 1971 |
|
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| PROCESS TESTING SERVICEABILITY OF TWO-DEGREE-OF-FREEDOM GYRO WITH ELECTRIC SPRING | 1994 |
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| METHOD OF INITIAL ORIENTATION FOR SPACECRAFT | 2000 |
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| GYROSCOPIC DEVICE FOR MEASURING PARAMETERS OF MOTION | 1991 |
|
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| METHOD COMPENSATING FOR INERTIAL ERROR OF GYROSCOPIC COMPASS WHILE VESSEL IS MANEUVERING AND GYROSCOPIC COMPASS FOR ITS REALIZATION | 1997 |
|
RU2128822C1 |
