Optoelectronic Module
CAPABILITY
Detection and determination of the travel trajectory and tracking of the flying object in the real-time mode and in the mode of post-call data processing.
Specifications
| Root-mean-square instrumental error when azimuth and elevation defining the point object coordinates, provided the altitude is ≤60°: - in the real-time mode on the basis of data received through the TV tracking channel and night TC channel (provided it was installed in the theodolite post), max - in the mode of post-call processing of the TV measuring channel data by standard computer equipment of the device |
1,5' 12'' |
| Range fining: - by the flying object with area min. 4 m2 and albedo 0,2; provided MRV = 20 km - by the flying object with area min. 0,12 m2 and albedo 0,2; provided MRV = 30 km |
from 0,5 to 13 km from 0,5 to 10 km |
| Root-mean-square error when finding the range to the object by means of a laser rangefinder (provided it was installed in the theodolite post), m, max | 1 |
| Angular movement range of the azimuth-elevation rotary mechanism: - azimuth - altitude - subject to elevation mounting of the laser rangefinder woth the limits |
no limit -10° ... 190° -10° ... 70° |
| Angular rates of subjects tracking on the azimuth-elevation rotary mechanism axes | (0,3 ... 60) °/s |
| Maximal angular acceleration on the azimth-elevation rotary mechanism axes | 60 °/s |
| Power supply of the device from the three-phase fixed AC mains, V | 240/400 |
| Power consumption, kW, max | 8 |
