FIELD: aviation.
SUBSTANCE: invention relates to means for monitoring sights intended for teleorientation in the beam of machines and, in particular, of aircrafts using injection lasers as radiation sources. The claimed method for monitoring the sight of the teleorientation system with the radiating channels on injection lasers at the edge of the aircraft control strip comprises radiation through a diaphragm with a hole which is installed perpendicular to the optical radiation axis in the focal plane of the collimator lens, the radiation signal is removed by the recording device, with the help of which the radiation signal is converted into coordinates, and the sight parameters are evaluated. The diaphragm is made with a hole eccentric relative to its geometrical axis and displaced to the edge of the strip, and the axis of the diaphragm is aligned with the axis of the device laser radiation, wherein the diaphragm is rotated in a dynamic coordinate mode with a frequency of 0.5-1.5 Hz, the signal is removed by the recording device at the edge of the strip and the sight parameters are evaluated. The claimed method is implemented by the device for monitoring the sight parameters of the teleorientation system with radiating channels on injection lasers at the edge of the aircraft control strip and comprises a diaphragm located in the focal plane of the collimator lens, a photodetector device with electronic equipment connected to an electronic coordinate measuring equipment and coordinate extraction control equipment, a film holder cabinet for optical filters mounted on an optical bench. The diaphragm is made in the form of a disk with a hole which geometrical axis does not coincide with the geometrical axis of the disk mounted and fixed coaxially to the laser radiation of the device in a sleeve mounted on bearings in the gearbox housing with an electric motor and having a gear wheel which kinematically contacts the gear wheel connected to the electric motor shaft.
EFFECT: improved quality of sight parameter monitoring by ensuring maximum accuracy at the edge of the aircraft control strip.
2 cl, 4 dwg
