The flight control system of small multi rotor UAV is a compact flight control system developed for multi rotor aircraft. The flight control aircraft has the functions of detection, navigation control, mission planning and mission equipment control, and can control typical four rotor, six rotor, eight rotor and sixteen rotor aircraft.
The flight control system has the characteristics of small volume, light weight and low power consumption. At the same time, it provides rich external resources, can be flexibly configured, and has the advantages of multi platform compatibility.
Main functions
Attitude and navigation positioning function: the flight control system can provide accurate attitude and position information to ensure accurate and reliable aircraft flight control.
Rotor motor control function: the flight control system can provide 16 rotor motor control channels, which can be configured as four rotor aircraft, six rotor aircraft, eight rotor aircraft and sixteen rotor aircraft, and can also be configured according to user requirements.
Mission planning and management function: the flight control system has manual flight mode and automatic flight mode. In the automatic flight mode, it can realize autonomous navigation flight and execute corresponding flight management control according to the mission plan.
Mission equipment control and management function: the flight control system has a variety of common mission load control interfaces, which can control a variety of typical mission loads. The flight controller can automatically manage the mission loads according to the flight tasks.
Index
Size: 100mm (L) * 100mm (W) * 30MM (H)
Weight: 350g
Operating temperature: - 40 ℃ ~ 55 ℃
Power supply: DC 12V ~ 36V
Power consumption: ≤ 10W
Motor control channel: 16 channels
Data channel: 2-way 232 serial port, 2-way 422 serial port and 1-way can bus
Analog input channel: 4 channels
Analog output channel: 2 channels
Digital I / O channel: 4 channels
Satellite navigation: GPS Differential Positioning
