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AFC-2120 Small VTOL Fixed Wing Flight Control System

SKU: MD-P00392·Mission Payloads & Systems·Sob encomenda

AFC-2120 Small VTOL Fixed Wing Flight Control System
AFC-2120 Small VTOL Fixed Wing Flight Control System

Visão geral

Small fixed wing flight controller (VTOL) is a small flight control system developed for fixed wing VTOL UAV. The flight controller can be applied to 20 ~ 60kg fixed wing UAV. The flight controller has the functions of real-time attitude, position detection, navigation control, task planning and task equipment control. The flight control computer has the characteristics of small volume, light weight and low power consumption. At the same time, it provides rich external resources and can be configured flexibly. Attitude and navigation positioning function : the flight controller can provide accurate attitude and position information to ensure accurate and reliable aircraft flight control. Control the vertical takeoff and landing function of fixed wing aircraft : the flight control aircraft has the function of controlling the four rotor aircraft, and can control the vertical takeoff and landing of the aircraft through the four rotor mode; The flight control aircraft also has the function of controlling the aircraft to switch between four rotor aircraft mode and fixed wing aircraft mode. Mission planning and management function : the flight controller has manual flight mode and automatic flight mode. In the automatic flight mode, it can realize autonomous navigation flight according to the mission pre planned route, and execute corresponding flight management control according to the mission plan. Mission equipment control and management function : the flight control computer has a variety of common mission load control interfaces, which can control a variety of typical mission loads The flight control computer can The mission automatically manages the mission load. Size: 163mm (L) * 71mm (W) * 66mm (H) Operating temperature: - 40 ~ 55 Power supply: DC 12V ~ 36V Steering gear control channel: 8 channels

Especificação técnica

Specifications. Especificações principais: Size 163mm (L) * 71mm (W) * 66mm (H), Weight 650g, Operating temperature - 40 ~ 55, Power supply DC 12V ~ 36V, Power consumption 10W, Steering gear control channel 8 channels, Rotor motor control channel 4 channels, Data channel 2-way 232 serial port, 2-way 422 serial port, 1-way can bus, Analog input channel 8 channels, Analog output channel 2 channels, Digital I / O channel 4 channels, Satellite positioning GPS L1 GLONASS differential positioning + airborne differential direction finding.

Especificação técnica — 1 groups
Especificações principais: Size 163mm (L) * 71mm (W) * 66mm (H), Weight 650g, Operating temperature - 40 ~ 55, Power supply DC 12V ~ 36V, Power consumption 10W, Steering gear control channel 8 channels, Rotor motor control channel 4 channels, Data channel 2-way 232 serial port, 2-way 422 serial port, 1-way can bus, Analog input channel 8 channels, Analog output channel 2 channels, Digital I / O channel 4 channels, Satellite positioning GPS L1 GLONASS differential positioning + airborne differential direction finding.

Especificações técnicas

Specifications

Size
163mm (L) * 71mm (W) * 66mm (H)
Weight
650g
Operating temperature
- 40 ~ 55
Power supply
DC 12V ~ 36V
Power consumption
10W
Steering gear control channel
8 channels
Rotor motor control channel
4 channels
Data channel
2-way 232 serial port, 2-way 422 serial port, 1-way can bus
Analog input channel
8 channels
Analog output channel
2 channels
Digital I / O channel
4 channels
Satellite positioning
GPS L1 GLONASS differential positioning + airborne differential direction finding

Aeronaves compatíveis

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