Panda II adopts Integrated design, built-in high-precision barometer, MEMS gyroscope,
Digital accelerometers reduce redundant interfaces and reduce the difficulty of wiring installation.
Come with high-precision inertial navigation devices and high-speed attitude calculation processors, which can ensure flight stability, strong wind resistance, and high safety.
Aim to the surveying and mapping industry. RTK is supported and centimeter-level positioning accuracy is achieved.
Connect with FY-608 Data radio, communication distance can up to 30km.
Multiple safety protection measures are supported, such as height protection, no GPS signal
hovering, automatic return when the signal loss, etc., safeguarding the safety of aircraft.
Various take-off and landing modes are supported. Launching off, throw off, parachute landing, slide landing and so on.
Using high-performance SINS/GPS algorithms, flight attitude control in a high precision.
The Panda II's shell is made by aluminum alloy which can shield outside interference effectively.
compatibility : fixed wing
Output control surface servo : 3
Available waypoints : 98
GPS altitude accuracy : 2.0m
Range of ground speed measurement : 0~350km/h
GCS : support
Output throttle :1
POS recorded : support
GPS horizontal accuracy : 2.5m
Range of the altitude measurement : -500~6000m
Work voltage : DC 5 v
Power consumption : <1 w
Storage temperature : -20°C ~ 45°C
Working temperature :-20 ℃ ~ 45°C
Storage humidity : 5 % ~ 60 %
Working humidity : 10 % ~55 %