Purpose and area of application Equipment is applied for control and regulation of traffic, for remote surveillance of unmanned aerial flight vehicle landing.
It ensures surveillance and tracking to land, provides aircraft control information to assist its landing in the required region.
Technical characteristics
| Time of operation |
from morning to evening with illumination of 50 – 100000 Lux in observed zone |
| Tracking distance (in visibility conditions over 20 km): |
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Large target (dimensions over 40x80 m) |
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max. distance, km |
15 |
| |
min. distance, m |
100 |
| |
Small target (dimensions 3x3 m) |
| |
max. distance, km |
5 |
| |
min. distance, m |
20 |
| Field of vision (FV): |
| |
max FV |
18° (elevation) x 24° (azimuth) |
| |
min FV |
3° (elevation) x 4° (azimuth) |
| Scanning system of television signals |
CCIR, 25 frames per s., 525 lines, line interlacing. |
| Tracking mode |
tracking with correlation on section and centroid-based tracking |
| Information yield, per/s |
50 |
| Specifications of gyro-stabilized two-cardan servo-frame: |
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azimuth and elevation range, deg. |
±30 |
| |
max. tracking range, °/s |
20 |
| |
max. acceleration, °/s2 |
60 |
| Accuracy of stabilization and tracking when defining the field of vision on two axes in case of sine-shaped space orientation max. speed - 6,28°/s and max. acceleration - 40°/s2: |
| |
boresight stabilization error, deg., less than. |
0,4 |
| |
tracking error, deg. |
0,05 |
| Environmental conditions: |
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operation temperature, °C |
- 40…+55 |
| |
relative humidity (under 25°C), % |
95±3 |
| Overall dimensions: |
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diameter, mm |
180 |
| |
length, mm |
600 |
| |
optical window radius, mm, not exceeding |
80 |
| Weight, kg, not exceeding |
15 |
| DC power supply, V |
27 ± 3 |
| Consumption current, A, not exceeding |
4 |
Advantages The field of vision of controlled object can be changed from maximal to minimal and vice versa in either manual or automatic mode.
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