Technical Parameter

Flight Characteristics

Multi-Rotor Quad Plane Tilt Wing Fixed Wing Unmanned Vehicle Unmanned Surface Vehicle	Flight Time Low Power Joysticks lose GPS lose Engine lost Attitude Height Overrun Electric Fence Quad Plane Conversion Timeout Emergency Landing	Pod Tracking、Dynamic Take-Off and Landing/Recover*

Hardware Features

12V~53V	<15W	1440 DMIPS	-40℃~75℃	< 0.1°	0.2°	0.02 m/s	1cm + 1PPM	-8g~8g	Four redundant IMU Triple Redundant Directions (Dual Magnetic Compass+Dual Antenna)* Dual Redundant Satellite Receiver* Dual Redundant Airspeed Meter* Triple Redundant Barometer* Dual Processor Double Redundant Data Link*

I/O

Up to 19, 3.3 & 5	Up to 6, RS232 & RS42	Up to 3	1	1	2	3 BUS，0~58V

* Extended Functions