SENSOR UNIT Russian patent published in 2024 - IPC G01C19/58 G01C21/10 

FIELD: orientation and navigation systems.

SUBSTANCE: invention relates to the creation of orientation and navigation systems for aircraft. Centres of mass of six accelerometers of disclosed unit are arranged in pairs and symmetrically at a certain distance relative to centre of mass of aircraft, sensitivity axes are oriented along its orthogonal construction axes and perpendicular to corresponding centripetal accelerations. Outputs of the first and second accelerometers are connected to the first and second inputs of the first summing amplifier and the first subtracting amplifier, respectively, outputs of the third and fourth accelerometers are connected to the first and second inputs of the second summing amplifier and the second subtracting amplifier, respectively, outputs of the fifth and sixth accelerometers are connected to the first and second inputs of the third summing amplifier and the third subtracting amplifier, respectively, and outputs of first-third summing amplifiers are connected to inputs of first-third scaling units, respectively, outputs of the first-third subtracting amplifiers are connected to inputs of the first-third integration units, outputs of which are connected to inputs of the fourth-sixth scaling units.

EFFECT: broader functional capabilities.

1 cl, 2 dwg