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Redundancy Design, High Reliability, Fast Dynamic Response

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Dual-Redundancy Servo Controller

It is used for servo control over the electromechanical actuator or other electric mechanisms of the brushless DC motor (BLDC) and permanent magnet synchronous motor (PMSM) in the aircraft's steering system and mission system.

By virtue of the master architecture consisting of the sophisticated digital processor and programmable logic devices, high-tech digital servo technologies (current, rotating speed, and position control), and cutting-edge motor control algorithm (FOC), it can be applied in the servo system satisfying the demands for large loading capacity, high accuracy, and fast dynamic response.

Product Highlights

Master architecture consisting of the sophisticated digital processor and programmable logic devices

Applied in the servo system satisfying the demands for large loading capacity, high accuracy, and fast dynamic response

Technical Specifications

Power supply of 28 VDC, power ≤ 500 W

Power range

Hall sensors, encoder, rotary transformer, LVDT/RVDT, etc.

Flexible sensor applications

≤1%F.S

High-accuracy position control

50～20000RPM

Wide-range speed control

Applications

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Modification from 700 kg manned helicopter to unmanned platform

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R&D of 550 kg coaxial unmanned helicopter

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3-ton unmanned platform

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