FIELD: transport.
SUBSTANCE: device for control over spacecraft position in space with the help of orbital gyrocompass. Control device comprises local vertical plotter, adders, amplifier-converter units, integrators, compensation units and gyro meter of angular velocity, spacecraft position setting device, cosine angle transducers, sine angle transducers, spacecraft veering control unit and spacecraft bearing setting unit. Connection between device elements are configured to allow spacecraft turn the course through arbitrary angle without loss in orientation relative to orbital system of coordinates. Note here that contour of correction from local vertical plotter is in operating mode. Spacecraft can either spin along the course or stay in definite position relative to orbital system of coordinates with loss in precision of orientation.
EFFECT: higher precision of orientation.
5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| PLATFORM-FREE ORBITAL GYROCOMPASS WITH ARBITRARY COURSE ORIENTATION OF SPACECRAFT | 2011 |
|
RU2488774C1 |
| GYRO-COMPASS FOR ORBITAL SPACECRAFT | 2015 |
|
RU2597018C2 |
| 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 |
| 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 |
| SYSTEM OF RETURN OF COURSE ORIENTATION OF SPACE VEHICLE USING ORBITAL GYROCOMPASS | 2017 |
|
RU2676844C1 |
| 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 |
