FIELD: aircraft control equipment. SUBSTANCE: invention discloses specific orientation of sensitivity axes of seven accelerometers, connection of outputs of accelerometers to commutator, which provides their connection to inputs of adders and device outputs. In addition outputs of accelerometers are connected to inputs of adders, which outputs are connected to commutator and respective comparators, which inputs are connected to input zero line. Outputs of comparators are connected to decoder, which output line is connected to commutator. EFFECT: decreased weight and size of measuring equipment of aircraft control system due to eight-to-seven decrease in number of accelerometers. 3 dwg
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