FIELD: transport, space engineering.
SUBSTANCE: method of controlling the geostationary spacecraft orientation consists in determining the dependence upon spacecraft yaw angles of those of every receiving aerial polarisation plane turn. Note here that a pair of identical receiving aerials is arranged at the points adjoining one or several aiming points and receiving linearly polarised signals from the beacon. Note also that the beacon polarisation plane is aligned with the plane formed by the axes of localised basis, one of them being aligned with local vertical while the other one being aligned with the pitch angle control axis.
EFFECT: spacecraft yaw orientation controlled from onboard beacon by single radiating conductor without using other onboard transducers.
7 dwg
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