FIELD: instrument making.
SUBSTANCE: invention relates to aviation and space instrument making and can be used for spatial angular orientation of orbital spacecraft (OSC), in which orientation systems are used built on principle of orbital gyro compassing. For this purpose, it includes roll channel control module (ICC-K), unit for setting program motions (BPOA), module for program motions calculating (IRAP) and orientation channels interference compensation module (ICM), functional links between which enable SC to provide program turns simultaneously on heading, roll and pitch, while maintaining stable gyro compassing.
EFFECT: broader functional capabilities.
1 cl, 6 dwg
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