Supporting rotor and fixed wing, vertical takeoff and landing, running
takeoff and landing, catapult-assisted take-off and parachute landing
Using high-precision sensor with strong
anti-vibration ability and good stability.
Using high-performance GNSS/SINS/AHRS algorithm, AHRS mode is automatically
adopted when without satellite signal.
Temperature compensation of the sensor is carried out
in the range of -40°C ~ +85°C.
Integrating DGPS post processing system which can reduce the field image
control points by more than 80%.
Built-in high-capacity data memory, which can record flight log and raw data
of satellite for more than 10 hours.
Built-in frequency hopping digital transceiver with a communication distance of up
to 60 km (sighting condition)
Dual-redundancy IMU, location and navigation system
Automatic route planning and automatic creation of take-off and landing
route by triple-redundancy navigation system
