| 摘要 |
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 |
