FIELD: space.
SUBSTANCE: gyrocompass system of orientation of artificial Earth satellite (AES) includes infrared local vertical plotter roll channel, eight adders, three amplifying-transforming devices, a unit of gyroscopic angular velocity transducers (BDUS) over a roll, three integrators, BDUS heading channel, three orbital angular speed setting devices, pitch channel reference BDUS pitch channel, two coordinate converters, a program point angles setting device, differentiator, setting device for projections of orbital angular velocity on axis of roll and pitch AES connected in a certain manner.
EFFECT: providing AES orbital orientation during development of preset program point angles.
1 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF ORBITAL GYRO COMPASSING AND DEVICE THEREFOR | 2015 |
|
RU2583350C1 |
| METHOD OF SPACECRAFT ORIENTATION IN TRACK SYSTEM OF COORDINATES WITH GROUND OBJECT OBSERVATION HARDWARE DRIVE AND DEVICE TO THIS END | 2011 |
|
RU2497728C2 |
| GYROCOMPASS SYSTEM OF ORIENTATION OF ARTIFICIAL EARTH SATELLITE | 2012 |
|
RU2498216C1 |
| PLATFORM-FREE ORBITAL GYROCOMPASS WITH ARBITRARY COURSE ORIENTATION OF SPACECRAFT | 2011 |
|
RU2488774C1 |
| DEVICE TO CONTROL SPACECRAFT POSITION IN SPACE WITH HELP OF ORBITAL GYROCOMPASS | 2012 |
|
RU2509690C1 |
| METHOD OF ORIENTING SPACECRAFT USING GIMBALLESS ORBITAL GYROCOMPASS AND SYSTEM THEREFOR | 2014 |
|
RU2579387C1 |
| SYSTEM FOR CONTROLLING SPATIAL ORIENTATION OF SPACECRAFT USING GIMBALLESS ORBITAL GYROCOMPASS | 2015 |
|
RU2597015C1 |
| GYRO-COMPASS FOR ORBITAL SPACECRAFT | 2015 |
|
RU2597018C2 |
| CORRECTION METHOD AND ORBITAL GYROCOMPASS DEVICE DESIGNED FOR CONTROLLING SPACECRAFT ANGULAR MOTION | 2014 |
|
RU2579406C1 |
| METHOD OF COMPENSATING FOR ERRORS OF ORBITAL GYROCOMPASS | 2015 |
|
RU2597017C2 |
