FIELD: aviation.
SUBSTANCE: invention relates to the apparent motion control of spacecrafts (SC) with predominantly monoaxially rotating solar panels (SP). SC oriented along the local vertical during the flight rotates continuously on course, the SP are simultaneously and continuously turned to the sun with the normal. The algorithm of the SC and SP control is implemented by mathematical relations received in the final form. SC and SP angular spin rates at the moment of sunset are stored and saved to maintain SP orientation to the sun in the shadow areas of the orbit.
EFFECT: simplified and increased self-sufficiency of the spacecraft and solar battery controlling means.
2 cl, 3 dwg
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