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METHOD OF CONTROLING PRESENT STATUS OF SOLAR BATTERY OF A SPACECRAFT WITH INERTIATIVE END ORGANS

机译:控制末端有机物的航天飞机太阳能电池现状的方法

摘要

FIELD: airpower.;SUBSTANCE: method of controlling present status of solar battery panel (SB) of the spacecraft (SC) includes the orientation of the SB working surface to the Sun, the measurement of the current values from the SB, the monitoring of the present state of SB based on the comparison of the present measured current values and current values measured in the previous flight stages. Control of SB panel status is performed by comparing the obtained current values from SB, each of which is multiplied by the ratio of squares of the current value of the distance from the Earth to the Sun and the average distance from the Earth to the Sun determined at the time of corresponding current measurement.;EFFECT: increase the accuracy of assessing the current efficiency of solar battery, providing the same conditions for measuring the current from the solar battery against the background of space flight of spacecraft in an orientation in which the total external disturbance moment for the turn reaches a minimum value.;1 cl
机译:领域:空中力量;物质:控制航天器(SC)的太阳能电池板(SB)当前状态的方法包括SB工作表面相对于太阳的方向,从SB的电流值的测量,监测SB的当前状态基于当前测量的电流值与先前飞行阶段中测量的电流值的比较。通过比较从SB获得的电流值来执行SB面板状态的控制,将每个电流值乘以确定的从地球到太阳的距离的当前值与从地球到太阳的平均距离的当前值的平方之比效果:提高评估太阳能电池电流效率的准确性,提供了在航天器航天飞行背景下以相同方向测量来自太阳能电池的电流的相同条件转弯的外部干扰力矩达到最小值。; 1 cl

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