H1helicopter flight control adopts high-precision inertial navigation unit,with omnidirectionalGNSpositioning technology,
complex attitude can be achieved(inverted flight)accurate attitude calculation under the environment。
provide pure manual,GPSfixed point and fixed height,about semi-autonomous flight,return and other modes,
support power detection,low power return can be achieved。
6.4-8.4V,electric adjustmentBECpower supply(can't be used5V BEC)
size
main controller:31.4mm*48.5mm*18.5mm
GPSmodule:39mm*46mm*15mm
operating ambient temperature
-10℃至55℃
weight
main controller:38.7g
GPSmodule:28.1g
hovering accuracy(GPSmode)
vertical:±0.5m,horizontal:±1.5m
maximum wind resistance
10m/s
maximum yaw angular speed
stunt mode300°/s
maximum tilt angle
45°(default35°)
maximum rising speed
4m/s
maximum falling speed
4m/s
*various parameter values listed on this page,all in mass production H1measured in a controlled test environment,in different external environments,use mode,under firmware version,results may vary in varying degrees,please subject to actual experience。