FIELD: astronautics.
SUBSTANCE: invention relates to space engineering, particularly to methods of controlling orientation and stabilization of a spacecraft. Method of dynamic high-accuracy orientation and stabilization of a spacecraft consists in using gyrodynes as actuators, which enable to provide control of a spacecraft at turns of SC on specified angles by roll, yaw and pitch. In high-dynamic mode, an engine is used in the gyro control drive, the shaft of which is connected directly to it. To stabilize the spacecraft, an engine is used in the gyro control drive, the shaft of which is connected to it via a reduction gear.
EFFECT: enabling switching of high-dynamic mode of operation of gyrodyne to a mode with high stabilization, and vice versa.
1 cl, 2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF CONTROLLING MOVEMENT OF SPACECRAFT WITH CONTROLLED ORIENTATION | 2020 |
|
RU2767648C1 |
| COMBINED GRAVITATIONAL ORIENTATION SYSTEM OF A SMALL SPACECRAFT | 2016 |
|
RU2658070C2 |
| METHOD OF CONTROLLING SPACECRAFT FOR REMOTE EARTH SENSING | 2019 |
|
RU2722598C1 |
| METHOD OF SPACECRAFT ORIENTATION AND DEVICE FOR THE METHOD REALISATION | 2016 |
|
RU2618664C1 |
| METHOD AND DEVICE FOR CONTROLLING MOTION OF A SPACECRAFT WITH CONTROLLED ORIENTATION | 2017 |
|
RU2669481C1 |
| METHOD OF ESTIMATION OF POSITION OF CENTER OF MASS OF SPACECRAFT IN COURSE OF ITS CONTROL BY MEANS OF POWER DRIVES | 1997 |
|
RU2114031C1 |
| DEVICE FOR CONTROLLING MOTION OF A SPACECRAFT FOR CLEANING SPACE FROM GARBAGE DEBRIS | 2016 |
|
RU2676592C2 |
| METHOD FOR CORRECTING THE ORBITAL MOTION OF A SPACE VEHICLE | 2022 |
|
RU2787522C1 |
| METHOD FOR CORRECTING THE ORBITAL MOTION OF A SPACECRAFT | 2021 |
|
RU2767794C1 |
| METHOD FOR SPACECRAFT ORIENTATION CONTROL EQUIPPED WITH AN ONBOARD RELAY COMPLEX | 2021 |
|
RU2761363C1 |
