FIELD: transport, space engineering.
SUBSTANCE: system designed to determine spacecraft solar battery maximum output comprises a unit to measure the angle between direction to the Sun and spacecraft orbit plane, unit to measure the spacecraft altitude, unit to measure spacecraft angular velocity, unit to define the orbit enlightened section beginning, unit to determine time intervals allotted for determination of solar battery maximum output, time oscillator, comparator unit and key.
EFFECT: ruling out negative influence of radiation reflected from Earth surface.
7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| METHOD FOR DETERMINING MAXIMUM SPACE VEHICLE SOLAR BATTERIES POWER OUTPUT, AND SYSTEM USED FOR METHOD REALISATION | 2006 |
|
RU2353555C2 |
| METHOD OF DETERMINING SPACECRAFT SOLAR BATTERY MAXIMUM OUTPUT | 2007 |
|
RU2354592C2 |
| METHOD OF COSMIC VEHICLE SOLAR BATTERIES POSITION CONTROL AND SYSTEM FOR ITS IMPLEMENTATION | 2006 |
|
RU2340518C2 |
| SYSTEM OF CONTROL OF SPACECRAFT SOLAR BATTERIES POSITION | 2006 |
|
RU2341421C2 |
| METHOD OF SPACECRAFT SUN BATTERIES POSITION CONTROL AND SYSTEM OF ITS IMPLEMENTATION | 2006 |
|
RU2325312C2 |
| METHOD OF CONTROL OF SPACECRAFT SOLAR BATTERY POSITION AND SYSTEM FOR REALIZATION OF THIS METHOD | 2005 |
|
RU2322374C2 |
| METHOD OF SPACECRAFT SUN BATTERIES POSITION CONTROL AND SYSTEM FOR ITS IMPLEMENTATION | 2005 |
|
RU2325311C2 |
| METHOD OF CONTROL OF SPACECRAFT SOLAR BATTERY POSITION AND SYSTEM FOR REALIZATION OF THIS METHOD | 2005 |
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RU2322372C2 |
| METHOD OF CONTROL OF SPACECRAFT SOLAR BATTERY POSITION AND SYSTEM FOR REALIZATION OF THIS METHOD | 2005 |
|
RU2322373C2 |
| METHOD FOR CONTROL OF POSITION OF SOLAR BATTERIES OF SPACE VEHICLE AND SYSTEM FOR ITS REALIZATION | 2003 |
|
RU2242408C1 |
