FIELD: physics; control.
SUBSTANCE: invention relates to controlling spacecraft motion using a correction jet engine. The method includes applying test and corrective action to the spacecraft. For each said actions, the rate of heating of the walls of the combustion chamber of the correction engine is determined. A transformation coefficient is determined from test data (trust and rate of heating). The thrust of the correction engine is calculated by multiplying said coefficient with the rate of heating for corrective action. A set of accurate correction values for further operation of the spacecraft is obtained by processing correction plans.
EFFECT: high quality of maintaining (including reliability and rapid correction) spacecraft in a given region, particularly on a geostationary orbit.
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR CORRECTING THE ORBITAL MOTION OF A SPACECRAFT | 2021 |
|
RU2767794C1 |
| METHOD FOR CORRECTING THE ORBITAL MOTION OF A SPACE VEHICLE | 2022 |
|
RU2787522C1 |
| METHOD FOR CORRECTING THE ORBITAL MOTION OF A SPACECRAFT | 2021 |
|
RU2762586C1 |
| METHOD OF SPACE VEHICLE ORBITAL MOVEMENT CORRECTION ACTION | 2015 |
|
RU2624889C2 |
| METHOD OF SPACECRAFT ORBITAL FLIGHT CORRECTION | 2012 |
|
RU2496689C1 |
| METHOD OF RETAINING GEOSTATIONARY SPACECRAFT IN PRESET ORBITAL POSITION | 2011 |
|
RU2486111C1 |
| SPACE VEHICLE CORRECTION ENGINE TEST METHOD | 2012 |
|
RU2535352C2 |
| METHOD OF SPACECRAFT ORBITAL FLIGHT CORRECTION | 2011 |
|
RU2496688C2 |
| DEVICE FOR DETERMINATION OF THRUST OF STATIONARY PLASMA ENGINE | 2022 |
|
RU2786669C1 |
| METHOD OF RETAINING GEOSTATIONARY SPACECRAFT IN PRESET ORBITAL POSITION | 2011 |
|
RU2481249C2 |
