INERTIAL TRANSDUCER Russian patent published in 2024 - IPC G01P15/08 G01C21/16 

FIELD: control systems.

SUBSTANCE: invention relates to aircraft control systems with excess number of meters. Unit of micromechanical accelerometers and micromechanical angular velocities additionally includes uniaxial micromechanical accelerometers and micromechanical angular velocity sensors, electronic computing unit, inputs of which are connected to outputs of microcontrollers of unit of micromechanical accelerometers and micromechanical sensors of angular velocities, temperature sensors, converters of signals of micromechanical accelerometers and micromechanical angular velocity sensors, non-volatile memory unit. At that, electronic computing unit contains microcontroller of micromechanical accelerometers, microcontroller of micromechanical angular velocity sensors, microprocessor, inputs/outputs of microprocessor are connected to inputs/outputs of microcontrollers and converters of signals of micromechanical accelerometers and micromechanical sensors of angular velocities, with outputs of temperature sensors of inertial measuring unit, non-volatile memory, with outputs of satellite navigation system.

EFFECT: high accuracy of the inertial measuring device.

1 cl, 1 dwg