FIELD: instrument making.
SUBSTANCE: structure of a platform-free orbital gyrocompass (PFOGC) comprises additional blocks and links, which make it possible to rotate a spacecraft according to the course by an arbitrary angle without loss of accuracy in SC orientation relative to the orbital system of coordinates (OSC), leaving the correction circuit from LVB in the working mode. Stabilisation of the spacecraft (SC) is carried out relative to the program system of coordinates (PSC). The SC may either freely rotate according to the course with a speed, or be in a certain position relative to the OSC according to the course, without loss of orientation accuracy. At the same time the PFOGC will operate in the correction mode from the local vertical builder (LVB) and continue building of the instrumental OSC without interruption.
EFFECT: improved accuracy.
1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| DEVICE TO CONTROL SPACECRAFT POSITION IN SPACE WITH HELP OF ORBITAL GYROCOMPASS | 2012 |
|
RU2509690C1 |
| SYSTEM FOR CONTROLLING SPATIAL ORIENTATION OF SPACECRAFT USING GIMBALLESS ORBITAL GYROCOMPASS | 2015 |
|
RU2597015C1 |
| METHOD OF ORIENTING SPACECRAFT USING GIMBALLESS ORBITAL GYROCOMPASS AND SYSTEM THEREFOR | 2014 |
|
RU2579387C1 |
| GYRO-COMPASS FOR ORBITAL SPACECRAFT | 2015 |
|
RU2597018C2 |
| METHOD OF ORBITAL GYRO COMPASSING AND DEVICE THEREFOR | 2015 |
|
RU2583350C1 |
| METHOD OF COMPENSATING FOR ERRORS OF ORBITAL GYROCOMPASS | 2015 |
|
RU2597017C2 |
| CORRECTION METHOD AND ORBITAL GYROCOMPASS DEVICE DESIGNED FOR CONTROLLING SPACECRAFT ANGULAR MOTION | 2014 |
|
RU2579406C1 |
| METHOD OF SPACECRAFT ORIENTATION IN TRACK SYSTEM OF COORDINATES WITH GROUND OBJECT OBSERVATION HARDWARE DRIVE AND DEVICE TO THIS END | 2011 |
|
RU2497728C2 |
| GYROCOMPASS ORIENTATION SYSTEM FOR ARTIFICIAL EARTH SATELLITE | 2014 |
|
RU2579384C1 |
| GYROCOMPASS SYSTEM OF ORIENTATION OF ARTIFICIAL EARTH SATELLITE | 2012 |
|
RU2498216C1 |
