A Fault Tolerance System of Magnetic Suspension Control Moment Gyro High Speed ​​Rotor Inverter

A technology for controlling torque gyroscopes and high-speed rotors, applied in control systems, excitation or armature current control, motor control, etc., can solve problems such as fault-tolerant control of power tubes of BuckDC-DC converters, burning windings, and burning windings, etc. Achieve the effect of avoiding fault isolation and system reconstruction time, improving system reliability, and avoiding secondary faults
CN104135216BActive Publication Date: 2016-08-17安徽华驰动能科技有限公司

Patent Information

Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
安徽华驰动能科技有限公司
Publication Date
2016-08-17

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Abstract

A fault tolerant topology structure of a high-speed rotor inverter of a magnetic suspension control torque gyroscope is mainly composed of a Buck DC-DC converter with a redundancy tube, a four-leg phase redundancy inverter, a fault protection circuit, a small armature and inductance permanent magnet brushless DC motor and the like. According to the characteristics of the small armature and inductance permanent magnet brushless DC motor, the redundancy topology structure is designed based on a motor drive circuit with the Buck DC-DC converter and a three-phase full-bridge inverter, reliability of a high-speed rotor drive circuit of the magnetic suspension control torque gyroscope is improved, and fault tolerant control is achieved after a power tube is disconnected or short-circuits; meanwhile, a drive system has the advantage of low power consumption before and after a fault happens, and the structure has high application value for spacecrafts paying attention to low power consumption and high reliability.
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Description

technical field

[0001] The invention relates to a fault-tolerant system of a magnetic levitation control moment gyro high-speed rotor inverter, which is used for the fault-tolerant control of a permanent magnet brushless DC motor with a small armature inductance, and is especially suitable for the high reliability of the driving parts of the attitude control actuators of satellites and space stations. control. Background technique

[0002] Space applications require high precision, high torque, low power consumption, high reliability and long life for attitude control actuators. The magnetic levitation control moment gyroscope has the advantages of no friction and wear, no lubrication, long life, and high precision through active vibration control because its high-speed rotor is supported by magnetic levitation. It is an important attitude control actuator on the spacecraft. The high-speed rotor of the magnetic levitation control torque gyro is driven by a brushless DC moto...

Claims

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