FIELD: astronautics.
SUBSTANCE: invention relates to rocket engineering. Device for determination of spatial orientation of Soyuz-2 space rocket, with installed on-board standard units of navigation equipment of consumer and triaxial gyrostabilizer, comprises unit of angular speeds sensors, which inputs are directly connected to on-board digital computer. Unit of angular velocity sensors includes a unit of sensitive elements consisting of at least three accelerometers.
EFFECT: higher accuracy of orientation.
1 cl, 1 dwg
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