| 摘要 |
FIELD: military equipment, in particular, flight control systems. SUBSTANCE: the attitude stabilization device of jet projectile has an angular deflection sensor with signal and reference windings, sensing element provided with a permanent magnet and coupled to an electric drive, actuator and a signal converter, whose inputs are connected to the signal and reference windings, and the output- to the actuator. The device additionally uses a linearization voltage generator, the output of the signal converter is provided with series-connected adder and comparator, the angular deflection sensor is provided with an electric drive speed regulator and a cylindrical magnetic core positioned symmetrically relative to the center of the sensing element coaxially with the axis of its rotation, the signal and reference windings are installed between the sensing element and the cylindrical magnetic core, and the output of the linearization voltage generator is connected to the adder. EFFECT: enhanced precision of attitude stabilization. 1 dwg |
