Evo II RTK Chinese Unmanned Aerial Vehicle (UAV)
Evo II RTK
VTOL Unmanned Aerial Vehicle (UAV)
Other
Basic Information
Name
Evo II RTK Chinese Unmanned Aerial Vehicle (UAV)
Designation
Evo II RTK
Alternate Designation
Evo II RTK
Equipment Type
VTOL Unmanned Aerial Vehicle (UAV)
Manufacturer
Autel Robotics
Date of Introduction
2021
Description
The Evo II RTK Chinese Unmanned Aerial Vehicle (UAV)series integrates an entirely new RTK module, which provides real-time centimeter-level positioning data and supports Post-Processing Kinematic (PPK). The aircraft can record the original satellite observation data, camera exposure parameters, and various other data. The positioning system supports the A-RTK base station and RTK network, which helps to achieve accurate and stable data acquisition in complex operating environments.
Air & Air Defense Specifications
Engine
Electric
Endurance
36.00 hrs
System
Alternate Designation
Evo II RTK
Type
Vertical Take-Off and Landing (VTOL) Unmanned Aerial Vehicle (UAV)
Manufacturer
Autel Robotics
Crew
Unmanned
Operating Frequency
non-Japan：2.400 GHz - 2.4835 GHz；5.725 - 5.850 GHz
Japan：2.400 GHz - 2.4835 GHz；5.650 - 5.755 GHz
Transmission Power
2.4GHz
FCC/ISED：≤27dBm
SRRC/CE/MIC/RCM：≤20dBm
5.8G (non-Japan) ; 5.7G (non-Japan)
FCC/ISED/SRRC/MIC：≤27dBm
CE/ RCM：≤14dBm
Image position compensation
The position of the camera center relative to the phase center of the airborne A-RTK antenna, under the body axis system: (-2.63, 0.31, 83.5) mm, and the photo EXIF coordinates have been compensated. The positive XYZ axis of the body axis system points to the front, right, and bottom of the aircraft respectively.
GPS
GPS+BeiDou+Galileo（Asia）
GPS+GLONASS+Galileo（Other areas）
Gimble
Three-axis stabilization
Launching System
Vertical Take-Off and Landing (VTOL)
Recovery System
Vertical Take-Off and Landing (VTOL)
Operating Temperature
-10℃ ~ 40℃
Dimensions
Wheelbase
397 mm
Height
INA
Weight (with propeller and battery)
1,250 g
Maximum Takeoff Weight
INA
Automotive
Engine Name
INA
Engine Type
Electric
Engine Power
INA
Max Ascent Speed
5 m/s (automatic flight）
8 m/s (manual control）
Max descent speed
4 m/s
Max Horizontal Flight Speed
72 km/h
Max Tilt Angle
33°
Max Angular Velocity
120°/s
Maximum Service Ceiling Altitude
6,000 m
Hovering Accuracy
When RTK is enabled and working normally:
Vertical: ±0.1 m; Horizontal: ±0.1 m
RTK is not enabled: vertical: ±0.1 m (when the visual positioning is working normally);
±0.5 m (when GNSS positioning works normally)
Level: ±0.3 m (when the visual positioning is working normally);
±1.5 m (when GNSS positioning works normally)
Maximum Resistance to Wind
Level 8
Endurance
36 min
Details
Country of Origin
China
Category
Very Low-Cost, Close-Range UAVs (Less than 5 km Range)
Air > Very Low-Cost, Close-Range UAVs (Less than 5 km Range)
Filter Label
E
Classification
Domain
Air & Air Defense
Equipment Status
Active
Dimensions
Length
—
Width
—
Height
—
Weight
1.25 kg
Operators (1)
China
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