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A three-redundancy dual-drive motor control platform and control method

A motor control, dual drive technology, applied in the direction of motor control, AC motor control, control system, etc., can solve the problems of the motor control system working with a disease, unable to judge whether the self and the other channel are working normally, etc.

Active Publication Date: 2021-07-06
XIAN AVIATION COMPUTING TECH RES INST OF AVIATION IND CORP OF CHINA
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  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

[0005] When a fault occurs in the platform architecture of the digital motor controller using dual redundancy, it can only switch to the internal working state of each channel to deal with the fault. When the collected external signals are inconsistent (that is, external faults), the architecture cannot distinguish itself and Whether the other channel is working normally will cause the motor control system to "work with a disease"

Method used

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  • A three-redundancy dual-drive motor control platform and control method
  • A three-redundancy dual-drive motor control platform and control method
  • A three-redundancy dual-drive motor control platform and control method

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Embodiment Construction

[0049] The present invention will be further described below in conjunction with accompanying drawing:

[0050] Such as figure 1 As shown, a triple-redundancy dual-drive motor control platform includes three independent control channels (channel A, channel B, and channel C in the figure) and two independent drive channels (drive A and drive B in the figure). ;

[0051]Each independent control channel is used to collect and convert the phase current information and position information output by the sensor of the controlled motor, and receive the transmission from the external host computer through the bus (the bus is 1553B bus or RS422 bus or RS232 bus or other common industrial buses) Combined with the corresponding motor control algorithm, two initial control signals are generated, and the two initial control signals are passed through the cross transmission link (the protocol implementation method of the cross transmission link can be Manchester code or UART or other commo...

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Abstract

The invention discloses a three-redundancy dual-drive motor control platform and a control method. The platform includes three independent control channels and two independent drive channels; its main control steps are: 1. The three independent control channels are first synchronized to ensure that the tasks are executed at the same time; 2. Obtain the two channels of each independent control channel Initial control signal; 3. Determine two final control signals of each independent control channel; 4. Use the final control signal to power the controlled motor to realize motor control. The present invention enables the motor control system to have internal and external fault detection and processing capabilities from the motor control platform level, greatly improves the reliability of the motor control system, and avoids the occurrence of "sick work" of the motor control system.

Description

technical field [0001] The invention belongs to the field of aviation AC and DC motor control systems, and in particular relates to a three-redundancy dual-drive motor control platform and a control method. Background technique [0002] In the design of aviation AC and DC motor control system, the design of the motor controller is particularly important, and it is the core component of the entire control system. At present, most of the control systems use digital motor controllers. When it comes to the control of AC and DC motors, the key components of aircraft systems, combined with the characteristics of the motor itself (winding composition form and working mode), the design of digital motor controllers is reliable. Higher requirements are put forward in terms of performance and fault detection isolation effect. [0003] The platform architecture of the current digital motor controller is mostly single redundancy or double redundancy; [0004] When the single-redundancy...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02P23/00H02P25/18H02P29/024H02P29/028
CPCH02P23/00H02P25/18H02P29/027H02P29/028
Inventor 刘源白洁张弛
Owner XIAN AVIATION COMPUTING TECH RES INST OF AVIATION IND CORP OF CHINA
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