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