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Государственное внешнеторговое
унитарное предприятие
"Белспецвнештехника"
Адрес:
Республика Беларусь, 220103
г. Минск, ул. Калиновского, д. 8
Тел: +375 (17) 269-63-33
Факс: +375 (17) 269-63-43
E-mail: mail@bsvt.by
Время работы предприятия:
Понедельник - пятница
8.30-17.30
Обед:
13.00-13.45
Каталог
Air equipment and armament
Aircraft Helicopters Aircraft ECM Repair of aviation equipment Unmanned aerial vehicles Aviation means of destruction Airfield meteorological stations Aviation training center Control - diagnostic and measuring systems Aircraft training systems (ATS)Air defense
Radar reconnaissance means Unified air defense system Anti-aircraft missile weapons Automated control systems Radio electronic warfare and reconnaissance means Communication means Metrological systems Automated means for diagnostics and repair of radio electronic devicesAutomatic control system of UAV
The automatic control system of unmanned aerial vehicle (code “SAU-9.0 MINI”) is designed for automatic, automated and manual controls:
• UAV heavier than air with electrical power plant, takeoff by hand and parachute landing;
• UAV heavier than air with ICE, running takeoff and landing;
• UAV lighter than air (airship), equipped with cruise and (or) lifting electric motor.
“SAU-9.0 MINI” contents:
“SAU-9.0 MINI” is a complex autonomous soft hardware system consisting of:
• Equipment installed in aerial vehicle (monoblock, satellite navigation system, airborne central processor, device data reception and transmission; airborne antenna, pitot tube (PT), PT data processing unit);
• And ground control unit (computer, ground data reception and transmission unit, antenna, extended control panel, custom software).
Technical characteristics:
• Sensor types: accelerometers, gyroscopes, magnetometers, pitot-static tubes,
temperature sensor;
• Type of navigation receiver: GPS/GLONASS. Frequency of data refreshing no less than 5 Hz;
• Height range: form 0 to 5000 m;
• Speed range: from 0 to 300 km/h;
• Range of UAV orientation angle measurement: heading from 0 to 360°, roll ±180°, pitch ±90°;
• Range of measurement of UAV angular speed: ± 200°/s;
• Range of measurement of UAV linear acceleration: ± 6 м/с 2;
• Accuracy of UAV orientation angle: no more than 0.3°;
• UAV co-ordinate error in the SRNS correction mode: no more than 10 m;
• Accuracy of flight height stabilization: no more than 3-5 m;
• Quantity of flight mission points: 100;
• Power supply voltage: from 9 to 30 V.
