FIELD: physics.
SUBSTANCE: to achieve the specified result the inertial-satellite navigation system contains multichannel radio receiver input of which through the amplifier is connected to the antenna, and its outputs are connected to the first set of inputs of satellite location detector. Setup block of satellite data almanac is connected through outputs to the second set of inputs of satellite location detector. The timer is connected through output to synchronising input of satellite location detector, and its outputs are connected to inputs of radio visible satellite separator. Thus system fault tolerance is increased due to reservation of functions of satellite data processing units.
EFFECT: increased accuracy and fault tolerance.
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