FIELD: advertisement. SUBSTANCE: the method consists in placement of sources of reflected light flux on space orbits by injection of these sources of reflected light flux to the flight trajectory around the inner attraction body, displacement of each source of reflected flight flux to the formation flight trajectory, imparting pulses, corresponding to the placement of the projections of the sources of the reflected light flux on the celestial sphere, to the sources of reflected light flux, bringing the sources of reflected light flux to the operating position. The result is attained due to the fact that the sources of reflected light flux are imparted rotation and/or periodic variation of the reflecting characteristics. The device realizing this method has sources of reflected light flux located on board the flight vehicle with a means for imparting pulses to the sources of reflected light flux. Flat reflecting surfaces are used as sources of reflected light flux. EFFECT: simplified procedure. 3 cl, 3 dwg
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Authors
Dates
2001-05-10—Published
1997-02-12—Filed