Basic Parameters |
|
Flight Mode |
Attitude mode; GPS mode; AB point operation mode |
Applicable Models |
Quadcopter (Type I, II) Hexacopter (Type I, V, and IY Co-Axial Double-propeller, Type YI Co-Axial Double-propeller, Irregular-shaped 4-axis and 6-propeller) Octocopter (Type I, V, and X Co-Axis Double-propeller, Irregular-shaped 6-axis and 8-propeller) |
ESC |
PWM ESC with output lower than 490HZ |
Max. Output Channels |
8 |
RecommendedRemote |
PCM or 2.4GHZ, at least 8 channels remote controller |
Receivers |
S.BUS, PPM and PWM |
NO. ofCPU cores |
5-core |
Protective Functions |
Semi-automatic operation mode AB point operation mode Breakpoint continued spraying function Flow control function Out of control or hovering or returning Low power alarm and return landing protection |
Flight Characteristics |
|
Hovering Precision |
Horizontal Direction: ±2m Vertical Direction: ±0.8m |
Max Angle of Inclination |
30° |
Max. Yaw Speed |
150°/s |
Max. Vertical Speed |
6m/s |
Wind Tolerance |
Sustained Wind: Scale 3 Gust: Scale 4 |
Electro-mechanical Characteristics |
|
Working Voltage |
2-12S |
Power Consumption |
<4W |
Operating Temperature |
10℃~60℃ |
Seismic Peak |
<1G |
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