Product overview
The system controls UAV flight control mechanisms and control surfaces. It returns actuator position, speed, current and status information to an upper computer.
The assembly contains one dual-redundancy servo controller and two dual-redundancy electric actuators. The carrier supplies 28 VDC control power and 270 V actuating power.
The system communicates with the upper computer through RS422 and CAN buses. It uses position commands and internal actuator sensor feedback to control actuator position.
Specifications
| Specification | Value & conditions |
|---|---|
| Assembly | One dual-redundancy servo controller and two dual-redundancy electric actuatorsFor the 270 V dual-redundancy actuator servo system. |
| Carrier power | 28 VDC control power and 270 V actuating powerProvided by the carrier's power supply. |
| Communication interfaces | RS422 and CANCommunication with the upper computer for position servo operation. |
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