FIELD: transport.
SUBSTANCE: invention relates to space engineering and may be used for docking of two space objects, one active and another passive. Active space objected is placed in reference orbit to define characteristics of approach pulses via nominal parameters of said reference orbit to be applied to active space object in initial orbit. Then, characteristics of approach pulses are defined from actual parameters of active space object and applied to next orbits.
EFFECT: faster approach to passive space object.
3 dwg, 1 tbl
| Title | Year | Author | Number |
|---|---|---|---|
| CONTROL MODE OF MOTOR OF AN ACTIVE SPACE OBJECT, MATED WITH A PASSIVE SPACE OBJECT | 2010 |
|
RU2441821C1 |
| METHOD OF CONTROLLING ACTIVE FLIGHT OF SPACE OBJECT TO BE DOCKED WITH PASSIVE SPACESHIP | 2010 |
|
RU2440281C1 |
| CONTROL METHOD FOR SPACESHIPS APPROACHING COOPERATIVE SPACE VEHICLE | 2016 |
|
RU2629644C1 |
| METHOD OF CONTROL OVER ACTIVE SPACE OBJECT TO BE DOCKED TO PASSIVE SPACE OBJECT | 2014 |
|
RU2562908C2 |
| METHOD FOR CONTROLLING THE MOVEMENT OF A SPACE OBJECT WHEN APPROACHING ANOTHER SPACE OBJECT | 2020 |
|
RU2759360C1 |
| SPACE OBJECT MOTION CONTROL METHOD IN CASE OF APPROACH TO ANOTHER SPACE OBJECT | 2017 |
|
RU2657704C1 |
| METHOD TO CONTROL MOTION OF DOCKED SPACE OBJECTS | 2014 |
|
RU2562902C1 |
| METHOD OF DETERMINING THE SEQUENCE OF FLIGHTS BETWEEN OBJECTS OF SPACE DEBRIS WITH A SIGNIFICANT DIFFERENCE IN THE LONGITUDE OF THE ASCENDING NODE OF THEIR ORBITS | 2018 |
|
RU2688120C1 |
| METHOD FOR DETERMINING THE SEQUENCE OF FLIGHTS BETWEEN SPACE DEBRIS OBJECTS IN THE VICINITY OF A GEOSTATIONARY ORBIT | 2020 |
|
RU2759026C1 |
| METHOD OF DETERMINATION OF STATE VECTOR OF PASSIVE SPACE OBJECT | 2013 |
|
RU2542836C2 |
