FIELD: physics.
SUBSTANCE: invention relates to methods of determining angular motion parametres of winged pilotless aircraft and can be used in controlling pilotless aircraft, maneuvering with different flight modes: ricochet, gliding and combined mode. According to the proposed method, if the sections of the ground surface are not even, the platform is stabilised parallel to the plane of the local horizon using gyroscopic devices, and with radio altimetres if the ground surface is even, and angular motion parametres of the pilotless aircraft are measured relative this platform.
EFFECT: increased accuracy of determining angular motion parametres of pilotless aircraft.
2 dwg
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