FIELD: aviation.
SUBSTANCE: method includes the construction of the inertial solar orientation of the space vehicle with a system of power gyroscopes, measurement of vectors and their kinetic moments, maintenance of this orientation with simultaneous unloading of gyroscopes. At the same time, in certain parts of the orbit, the operations of spinning the spacecraft, measuring and comparing with the maximum permissible level of the accumulator battery (AB) charge, monitoring the power balance of the spacecraft, unloading the power gyroscopes, charging the accumulator batteries from solar batteries are carried out in a certain combination with each other. These operations are linked to the processes of planned and unplanned Earth surface survey.
EFFECT: increase of the spacecraft resource.
6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD OF CONTROLLING SPACECRAFT FOR REMOTE EARTH SENSING | 2019 |
|
RU2722598C1 |
| METHOD OF CONTROLLING MOVEMENT OF SPACECRAFT WITH CONTROLLED ORIENTATION | 2020 |
|
RU2767648C1 |
| METHOD FOR CONTROL DESIGN OF SPACECRAFT WITH POWER GYROSCOPES AND ROTARY SOLAR PANELS | 2015 |
|
RU2614467C1 |
| METHOD OF DETERMINATION OF MAGNETIC MOMENT OF SOLAR BATTERIES OF SPACECRAFT PROVIDED WITH POWERED GYROSCOPE SYSTEM | 2000 |
|
RU2176972C1 |
| METHOD FOR CONTROLLING THE ORIENTATION OF THE SPACECRAFT | 2021 |
|
RU2760818C1 |
| METHOD OF ORIENTATION OF SPACECRAFT | 2020 |
|
RU2736522C1 |
| METHOD FOR INCREASING SERVICE LIFE OF STORAGE BATTERIES ON SPACECRAFTS | 2018 |
|
RU2689887C1 |
| METHOD OF CONTROL OF SPACECRAFT SOLAR BATTERY POSITION AND SYSTEM FOR REALIZATION OF THIS METHOD | 2005 |
|
RU2322374C2 |
| METHOD OF CONTROL OF SPACECRAFT POWER SUPPLY SYSTEM | 2005 |
|
RU2291819C2 |
| EQUIPPED WITH SOLAR BATTERIES SPACECRAFT CONTROL METHOD | 2018 |
|
RU2679094C1 |
