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Automatic Unmanned Aerial Vehicles (UAV) Systems
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Mini UAV System
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Operative UAV System is destinated for aerial intelligenceand reconnaissance missions of areas distanced from base location. Flight planning is realized directly before take-off. Aircraft is launched by hand-through. UAV starts flying around the set waypoints in automatic mode after climbing to the desired altitude. Video is transmitted to tracking station in real-time. Guaranteed distance of video transmitting of standard configuration is up to 3 km (depending on terrain profile and the height of receiving antenna). Transmitting equipment of increased distance can be installed if necessary.
Flight Control System provides safe return of UAV, approach guidance or activation of parachute system. As batteries are recharged the system is ready for reuse.
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| Wing Span |
1510 mm |
| Length |
1400 mm |
| Take-off weight |
3,750 kg |
| Payload weight |
0,600 kg |
| Rrange |
50 km |
| Endurance |
40 mm |
| Cruising speed |
75 km/h |
| Flight Altitude |
50-500 m (above the surface) |
| Engine |
Electrical |
Tactical UAV System
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Tactical UAV System is designated for aerial monitoring, reconnaissance and surveying missions.
The route can be planned both on-site and on-the-fly. The take off is possible both from launching machine and by takeoff run. UAV start passing the set waypoints in automatic mode after climbing to the desired altitude. Video is transmitted to tracking station in real-time within radio signal reach.
Flight Control System enables the photo camera trigger synchronization by time and coordinates. Special software allows to analyze flight data, download the pictures from the camera, split the pictures and make photographic plan of the area.
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| Wing Spread |
1920 mm |
| Length |
1650 mm |
| Take-off weight |
7 kg |
| Payload weight |
1,500 kg |
| Flight distance |
100...150 km |
| Flight duration |
1,5...2 hours |
| Cruising speed |
60...80 km/h |
| Flight Altitude |
50-1500 m (above surface) |
| Engine |
Combustion |
Automatic Flight Control and Navigation System is the main system which enables autonomous flight of UAV distanced from base location, without contact with operator, under IMC and restricted visibility. The system is developed and manufactured by TeKnol Ltd. It consists of INS, GPS receiver, autopilot module and allows the following features:
- Completely automatic flight along predesigned flight path;
- Automatic take-off and approach guidance;
- Safe flight of any type of UAV even under gusty wind;
- Stabilization of UAV attitude during flight;
- Stabilization of video camera;
- Telemetry information output (flight parameters and on-board equipment status);
- Automatic piloting out of site of view;
- Programmed control of on-board equipment;
- Minimal training requirements to the staff.
UAV automatic flight path and flown trajectory in typical survey flight
(plotted using data from Flight Data Recorder)
Pictures, taken by UAV's video camera from the altitude 150m matched with Google Earth satellite photography
| Suburban road |
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Urban area |
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Downloads
Automatic Unmanned Aerial Vehicles Systems
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