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AFC-1110 Flight Control System for Multi Rotor Drone

SKU: MD-P00391·Mission Payloads & Systems·Made to Order

AFC-1110 Flight Control System for Multi Rotor Drone
AFC-1110 Flight Control System for Multi Rotor Drone

Overview

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. 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. Size: 100mm (L) * 100mm (W) * 30MM (H) Operating temperature: - 40 ℃ ~ 55 ℃ Power supply: DC 12V ~ 36V Motor control channel: 16 channels Data channel: 2-way 232 serial port, 2-way 422 serial port and 1-way can bus

Technical specification

Specifications. Key specifications: 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.

Technical specification — 1 groups
Key specifications: 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.

Technical specifications

Specifications

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

Compatible aircraft

This part fits the following platforms.

Fitment data pending — contact us with your aircraft model.

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