FIELD: physics, instrument-making.
SUBSTANCE: invention relates to test engineering and can be used during experimental processing of spacecraft power supply systems. The automated workstation for investigating and testing spacecraft power supply systems comprises a solar panel simulator, an accumulator battery simulator, a load simulator, a control system and an adjustment and control apparatus. Power leads of the adjustment and control apparatus are connected to outputs of corresponding simulators. The solar panel simulator comprises a control unit and series-connected rectifier, controlled power supply and a circuit of parallel-connected current stabilisers. The load simulator comprises a current stabiliser control unit and a circuit of parallel-connected current stabilisers. The accumulator battery simulator comprises series-connected modules which include electrochemical current sources.
EFFECT: invention provides high accuracy of simulation and efficiency of testing the automated workstation.
2 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SPACE VEHICLE POWER SUPPLY SYSTEM SIMULATION STAND | 2007 |
|
RU2349518C1 |
| METHOD OF GROUND ENVIRONMENT OF SPACECRAFT POWER SUPPLY SYSTEM | 2017 |
|
RU2671600C1 |
| SPACECRAFT POWER SUPPLY SYSTEM CONTROL METHOD | 2018 |
|
RU2682725C1 |
| METHOD OF CONTROLLING SPACECRAFT POWER SUPPLY SYSTEM | 2014 |
|
RU2593760C9 |
| SELF-CONTAINED POWER SUPPLY SYSTEM | 2005 |
|
RU2317216C2 |
| METHOD OF CONTROLLING AUTONOMOUS POWER SUPPLY SYSTEM OF SPACECRAFT | 2015 |
|
RU2593599C1 |
| METHOD TO CONTROL POWER SUPPLY SYSTEM OF SPACECRAFT | 2013 |
|
RU2537389C1 |
| METHOD TO CONTROL AUTONOMOUS POWER SUPPLY SYSTEM OF SPACECRAFT | 2014 |
|
RU2572396C1 |
| SPACECRAFT POWER SUPPLY SYSTEM CONTROL METHOD | 2017 |
|
RU2675590C1 |
| SPACECRAFT POWER SUPPLY SYSTEM | 2016 |
|
RU2650875C2 |
