Dual-redundancy actuator system and control method
A dual-redundancy and steering gear technology, applied in aircraft transmission, aircraft power transmission, aircraft power devices, etc., can solve the problems that are not introduced, fault diagnosis and isolation are not carried out, and the design of dual-redundancy system is not given in detail. and other problems to achieve the effect of ensuring normal work, improving life and reliability
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[0027] Such as figure 1 As shown, the present invention includes a redundant drive controller part 1 , a steering gear part 2 and a steering surface part 3 . The redundant drive controller part 1 receives the given signal of the rudder surface position, and is controlled by the control method to drive the double-redundant brushless DC motor 4 in the steering gear to work, so that the turning angle of the rudder surface follows the given signal of the rudder surface position. In the present invention, the control power supply, drive power supply, motor winding, motor Hall sensor, position sensor, and power drive unit are designed for backup.
[0028] Wherein, the redundant drive controller part 1 includes a control surface position feedback conditioning unit 5, a control surface position given receiving unit 6, a DSP unit 7, a CPLD unit 11, an isolation circuit unit 12, a power drive unit 13, a current acquisition unit 8, Overcurrent protection auxiliary unit 9 and power syste...
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