Description
Tiguar is a fully integrated, state-of-the-art unmanned system that fits under the U.S. Federal Aviation Administration 55 lbs. regulation and meets Polish Civil Aviation Authority requirements rgarding UAVs. It is a high endurance, safe and modular systems that can be deployed for aerial inspection, monitoring and surveillance missions
Additional information
| Year of last update | 2016 |
|---|---|
| Sensor control | Y |
| Type of Camera | FPV, 30x Zoom |
| Type of Lidar | Yellowscan |
| Additional Sensors and additional information | Thermal, Infrated scanners |
| Build-in Stablilsation | Y |
| Exchangeable | Y |
| Sensor tilting to allow oblique views | Y |
| Ground computer included | N |
| Type of Ground computer | – |
| Real time image and video download link | Y |
| Correction services [PPK, RTK] | – |
| Type of software included | Block adjustment, Camera self-calibration, Flight planning, Photogrammetric software, Point cloud processing software |
| Flight planning software | – |
| Photogrammetric software | – |
| Point cloud processing software | – |
| Automatically Generated Products | 3D City Models, Point Clouds, 3D Landscape Models, DEMs, DTMs, Orthomosaics, NDVI maps |
| Additional information on software or automatically generated products | – |
| Transportation accessories | – |
| Included batteries and charger | – |
| More included products and spare parts | – |
| Onboard imaging/scanning devices | RGB Camera, Lidar, Additional sensors, Gimbal, NIR Camera, SWIR Camera |
| Other sensors and additional information | – |
| Typical applications | S&R, Geomodeling, Monitoring |
| Number of rotors | 1 |
| Platform | Aircraft |
| Brand | Tiguar, KEYHELP INT. |
| Max. payload [kg] | 25 |
| Max. stay in the air [min] | 1440 |
| Max. speed [km/h] | 144 |
| Propulsion | electric-gasoline |
| ø / wingspan [cm] | 401 |
| Height [cm] | 232 |
| Transport on human back | N |
| Type of IMU | – |
| Min. operation temperature [°C] | -20 |
| Max. operation temperature [°C] | +40 |
| Min. ø of launch/landing site [m] | 100 |
| Launching method | automatic takeoff |
| Automatic launch and landing | Y |
| Training provided | Y |
| Collision avoidance systems (CAS) | Y |
| Autonomous emergency landing | Y |
| Type of GNSS receiver and captured signals | – |
| Addres | KEYHELP INT. Dzialdowska 11/13 str. 01-184 Warsaw Poland |
