Description
Professional Mapping UAS
Specifications
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Environment
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Min. operation temperature [Ā°C]
-10
Max. operation temperature [Ā°C]
45
Max. wind speed [m/sec]
18
Max. humidity [%]
90
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Imaging/scanning devices
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Onboard imaging/scanning devices
RGB Camera
Type of Camera
Sony ILCE-QX1
Additional Sensors and additional information
Sensor Type: Exmor APS HD CMOS. Resolution: 20.1 MP. Lens: Voightlander. Focal Length: E 21mm. Aperture Control: F2.8. Imaging Resolution: 1.5 - 20cm GSD.
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Platform
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Platform
Aircraft
Brand
South
Max. stay in the air [min]
85
Max. speed [km/h]
75
Max. height above sea level [m]
4000
Propulsion
Electric pusher propeller, 12in, foldable
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Operation Characteristics and Safety
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Launching method
Hand Launch
Automatic launch and landing
Y
Autonomous emergency landing
Y
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Dimensions
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Ćø / wingspan [cm]
150
Height [cm]
13
Weight [kg]
1.55
Number of rotors
1
Transport on human back
Y
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Navigation Sensors
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Type of GNSS receiver and captured signals
L1/L2 (GPS, GLONASS, Galileo, BeiDou-2), 5Hz/20Hz/50Hz
Type of IMU
Gyroscope, Accelerometer
Other sensors and additional information
Barometer, Magnetometer. With GCP's Acquisition performance is down to 1cm (horizontal) and 3cm (vertical).
Correction services [PPK, RTK]
PPK
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General
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Typical applications
Aerial Mapping, Terrain Modelling
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Included software and automatically generated
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Type of software included
Flight planning, Photogrammetric software, Point cloud processing software
Flight planning software
AIRace
Automatically Generated Products
3D City Models, Point Clouds, 3D Landscape Models, DEMs, DTMs, Orthomosaics
Additional information on software or automatically generated products
Flight conditions and parameters can bemonitored via GCS software in realtime. Once another battery is replacedfor a second flight, the remainedskyway of previous mission would becontinued automatically.