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An intelligent control method for a fault-tolerant servo system for multi-electric aircraft and new energy vehicles

A technology for new energy vehicles and multi-electric aircraft, applied in motor control, motor generator control, electronic commutation motor control, etc., can solve the problems of motor performance that cannot meet specific needs, reliability is not high enough, and response is not fast enough. Achieve the effects of simple control method, enhanced robustness, and improved fault tolerance

Active Publication Date: 2022-04-12
苏州容昇电气科技有限公司
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  • Summary
  • Abstract
  • Description
  • Claims
  • Application Information

AI Technical Summary

Problems solved by technology

However, in the actual application of the traditional permanent magnet motor control method, there are still problems such as insufficient fast response, insufficient reliability, and insufficient motor performance to meet specific needs.

Method used

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  • An intelligent control method for a fault-tolerant servo system for multi-electric aircraft and new energy vehicles
  • An intelligent control method for a fault-tolerant servo system for multi-electric aircraft and new energy vehicles
  • An intelligent control method for a fault-tolerant servo system for multi-electric aircraft and new energy vehicles

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Embodiment Construction

[0033] The technical solutions in the embodiments of the present invention will be clearly and completely described below in conjunction with the accompanying drawings. Apparently, the described embodiments are only some of the embodiments of the present invention, not all of them. Based on the embodiments of the present invention, all other embodiments obtained by ordinary persons in the art without making creative efforts belong to the protection scope of the present invention.

[0034] Specific operations such as figure 1 As shown, an intelligent control method for a fault-tolerant servo system for a multi-electric aircraft and a new energy vehicle, the method includes the following steps:

[0035] Step 1: Collect three sets of three-phase winding current i of the fault-tolerant servo motor A1 i B1 i C1 , i A2 i B2 i C2 , i A3 i B3 i C3 , after performing coordinate transformation processing on them respectively, A 1 B 1 C 1 Winding current vector i s1 , A 2 B...

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Abstract

The invention discloses an intelligent control method for a fault-tolerant servo system for a multi-electric aircraft and a new energy vehicle, specifically: step 1, collecting the current and voltage of three sets of windings, and obtaining the motor current vector and voltage vector according to the switch state; step 2, Carry out self-calibration processing of the stator flux observer; step 3, process the torque observer; step 4, process the speed regulator; step 5, process the torque regulator; step 6, process the flux regulator; Step 7. Find the optimal switch vector table to realize motor control; Step 8. If a fault occurs, realize fault-tolerant operation of the motor through a fault diagnosis and fault-tolerant processor. An intelligent control method for a fault-tolerant servo system for multi-electric aircraft and new energy vehicles is simple and easy to implement, has high reliability, has self-correction and fast response functions, improves the dynamic response performance of the motor drive system, and enhances the robustness of the motor drive system sex.

Description

technical field [0001] The invention relates to the field of servo motor control, in particular to an intelligent control method for a fault-tolerant servo motor drive system. Background technique [0002] With the development of multi-electric, all-electric aircraft and hybrid and pure electric vehicles, the motor drive system has ushered in new development opportunities and challenges. In addition to requiring high power density and high efficiency, it also needs to have high output performance and high reliability. performance, which has become the key to the motor drive system. In the 1990s, the emergence of permanent magnet fault-tolerant motors and their control systems improved the safety and reliability of the system, and have now been applied to the aviation field. However, affected by electromagnetic interference, insulation aging, poor contact and other factors, some electrical faults often occur in the motor and power tube in the drive system, which can generall...

Claims

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Application Information

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Patent Type & Authority Patents(China)
IPC IPC(8): H02P21/14H02P21/18H02P21/20H02P29/028
CPCH02P21/141H02P21/18H02P21/20H02P29/028
Inventor 蒋雪峰李洁
Owner 苏州容昇电气科技有限公司