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CN103346721A - Thrust ripple suppressing method of primary permanent magnet linear motor - Google Patents

Thrust ripple suppressing method of primary permanent magnet linear motor Download PDF

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CN103346721A
CN103346721A CN2013102440270A CN201310244027A CN103346721A CN 103346721 A CN103346721 A CN 103346721A CN 2013102440270 A CN2013102440270 A CN 2013102440270A CN 201310244027 A CN201310244027 A CN 201310244027A CN 103346721 A CN103346721 A CN 103346721A
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permanent magnet
motor
linear motor
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赵文祥
许沈鼎
吉敬华
刘国海
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Jiangsu University
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Abstract

本发明公开一种初级永磁型直线电机的推力波动抑制方法,通过有限元仿真或转矩测试仪实测得到初级永磁型直线电机的定位力,对定位力的波形进行谐波频谱分析,确定定位力中基波与主要高次谐波分量;采用有限元仿真电机的空载反电势波形,计算出用于抵消定位力谐波分量的三相电流分量,使得附加电磁推与定位力中的基波与主要高次谐波分量的幅值相等且相位相反,对电流滞环矢量控制系统注入三相谐波电流,对永磁型直线电机的推力波动进行抑制;无需对电机本体进行改造,可以通过控制策略来实现,既可显著抑制电机推力波动,降低电机运行中的噪声,同时又保持了电机的空载磁势、推力输出能力等特性不变。

Figure 201310244027

The invention discloses a thrust fluctuation suppression method of a primary permanent magnet linear motor. The positioning force of the primary permanent magnet linear motor is obtained through finite element simulation or actual measurement of a torque tester, and the harmonic spectrum analysis is performed on the waveform of the positioning force to determine The fundamental wave and main high-order harmonic components in the positioning force; the no-load back EMF waveform of the motor is simulated by finite element method, and the three-phase current component used to offset the harmonic component of the positioning force is calculated, so that the additional electromagnetic push and the positioning force The amplitude of the fundamental wave and the main high-order harmonic components are equal and the phases are opposite. The three-phase harmonic current is injected into the current hysteresis vector control system to suppress the thrust fluctuation of the permanent magnet linear motor; there is no need to modify the motor body, It can be realized through the control strategy, which can significantly suppress the thrust fluctuation of the motor, reduce the noise during the operation of the motor, and at the same time keep the characteristics of the motor's no-load magnetic potential and thrust output capability unchanged.

Figure 201310244027

Description

初级永磁型直线电机的推力波动抑制方法Thrust fluctuation suppression method for primary permanent magnet linear motor

技术领域 technical field

本发明涉及一种初级永磁型直线电机技术,具体是抑制初级永磁型直线电机推力波动的控制方法,属于电机驱动与控制技术领域,适用于城市轨道交通等应用场合。 The invention relates to a primary permanent magnet linear motor technology, in particular to a control method for suppressing thrust fluctuations of a primary permanent magnet linear motor, belongs to the technical field of motor drive and control, and is suitable for urban rail transit and other application occasions.

背景技术 Background technique

随着永磁材料性能的不断提高和永磁直线电机设计制造技术的不断完善,永磁直线电机以其高性能、高稳定性、低噪音和高效率等特点在工业自动化和轨道交通等领域得到广泛应用。初级永磁型直线电机是一类新型永磁无刷直线电机,其结构特点是永磁体和电枢绕组都安置在初级动子上,次级结构简单,仅由导磁铁心组成,集成了直线感应电机结构简单、成本低与永磁直线同步电机功率密度高的优点,特别适用于长定子应用场合。然而在初级永磁型直线电机中,永磁体和双凸极结构的相互作用产生了较大的定位力,从而引起了电机运行过程中推力的波动,直接影响了电机在速度控制系统中低速性能和在位置控制系统中的高精度定位。 With the continuous improvement of the performance of permanent magnet materials and the continuous improvement of the design and manufacturing technology of permanent magnet linear motors, permanent magnet linear motors have been widely used in industrial automation and rail transportation because of their high performance, high stability, low noise and high efficiency. widely used. The primary permanent magnet linear motor is a new type of permanent magnet brushless linear motor. Its structural feature is that the permanent magnet and armature winding are placed on the primary mover, and the secondary structure is simple. It is only composed of a magnetic core and integrates a linear motor. The induction motor has the advantages of simple structure, low cost and high power density of permanent magnet linear synchronous motor, especially suitable for long stator applications. However, in the primary permanent magnet linear motor, the interaction between the permanent magnet and the doubly salient pole structure produces a large positioning force, which causes the thrust fluctuation during the operation of the motor, which directly affects the low-speed performance of the motor in the speed control system. and high-precision positioning in position control systems.

目前关于抑制初级永磁型直线电机推力波动的方法主要集中在对电机本体结构的优化设计上,比如在动子两端添加辅助齿、定子长度优化、定子和转子上开辅助槽等等。此类方法适用于电机本体结构的设计阶段,一般先通过计算机软件建立电机的有限元模型,再遵循特定的优化策略来调整电机的结构参数,以达到推力波动减小的效果。但是由于对结构的优化方法通常受到不同类型电机结构的制约,使得抑制推力波动的效果有限;另外由于对电机结构的修改,必然会对电机的空载反电势、功率输出能力等产生影响,同时也增加了制造成本,使得对电机本体结构的此类优化方法在实际产业化过程中有一定的局限性。 At present, the methods for suppressing the thrust fluctuation of the primary permanent magnet linear motor mainly focus on the optimal design of the motor body structure, such as adding auxiliary teeth at both ends of the mover, optimizing the length of the stator, opening auxiliary slots on the stator and rotor, and so on. This type of method is applicable to the design stage of the motor body structure. Generally, the finite element model of the motor is established through computer software, and then the structural parameters of the motor are adjusted according to a specific optimization strategy to achieve the effect of reducing thrust fluctuations. However, because the structure optimization method is usually restricted by different types of motor structures, the effect of suppressing thrust fluctuations is limited; in addition, due to the modification of the motor structure, it will inevitably affect the no-load back EMF and power output capability of the motor, and at the same time It also increases the manufacturing cost, so that this kind of optimization method for the structure of the motor body has certain limitations in the actual industrialization process.

发明内容 Contents of the invention

本发明的目的是提出一种初级永磁型直线电机的推力波动抑制方法,无需对电机本体进行改造,只需修改相关的控制软件,通过控制策略来抵消电机的定位力,从而达到抑制电机推力波动的效果,提高了电机的动态性能。 The purpose of the present invention is to propose a thrust fluctuation suppression method for primary permanent magnet linear motors, without modifying the motor body, only need to modify the relevant control software, and offset the positioning force of the motor through the control strategy, so as to suppress the thrust of the motor The wave effect improves the dynamic performance of the motor.

本发明采用的技术方案是:采用常规的电流滞环矢量控制系统,包括以下步骤: The technical scheme that the present invention adopts is: adopt conventional current hysteresis loop vector control system, comprise the following steps:

(1)通过有限元仿真或转矩测试仪实测得到初级永磁型直线电机的定位力                                                

Figure 2013102440270100002DEST_PATH_IMAGE001
,利用傅里叶级数逼近法对定位力的波形进行谐波频谱分析,确定定位力中基波与主要高次谐波分量;A k k次定位力谐波分量的幅值,φ k k次定位力谐波分量的相位角,
Figure 2013102440270100002DEST_PATH_IMAGE002
τ s 为电机初级动子极距,x是初级动子位移。 (1) The positioning force of the primary permanent magnet linear motor is obtained through finite element simulation or actual measurement of the torque tester
Figure 2013102440270100002DEST_PATH_IMAGE001
, use the Fourier series approximation method to analyze the harmonic spectrum of the waveform of the positioning force, and determine the fundamental wave and main high-order harmonic components in the positioning force; A k is the amplitude of the k -th harmonic component of the positioning force, φ k is the phase angle of the kth harmonic component of the positioning force,
Figure 2013102440270100002DEST_PATH_IMAGE002
, τ s is the pole distance of the primary mover of the motor, and x is the displacement of the primary mover.

(2)采用有限元仿真初级永磁型直线电机的空载反电势波形,确定空载反电势

Figure 735501DEST_PATH_IMAGE003
E m 为反电势幅值。 (2) Use finite element simulation to simulate the no-load back EMF waveform of the primary permanent magnet linear motor to determine the no-load back EMF
Figure 735501DEST_PATH_IMAGE003
, Em is the magnitude of the back EMF.

(3)根据附加电磁推力

Figure 2013102440270100002DEST_PATH_IMAGE004
以及附加电磁推力F′ PMk 与定位力中的基波与主要高次谐波分量的幅值相等且相位相反,
Figure 964225DEST_PATH_IMAGE005
Figure DEST_PATH_IMAGE006
Figure 806279DEST_PATH_IMAGE007
,计算出用于抵消k次定位力谐波分量的三相电流分量i ak (x)i bk (x)i ck (x): (3) According to the additional electromagnetic thrust
Figure 2013102440270100002DEST_PATH_IMAGE004
And the amplitude of the additional electromagnetic thrust F′ PMk and the fundamental wave in the positioning force and the main higher harmonic components are equal and the phases are opposite,
Figure 964225DEST_PATH_IMAGE005
Figure DEST_PATH_IMAGE006
Figure 806279DEST_PATH_IMAGE007
, calculate the three-phase current components i ak (x) , i bk (x) , i ck (x) used to offset the k -order positioning force harmonic components:

Figure DEST_PATH_IMAGE008
Figure DEST_PATH_IMAGE008
,

v为实测电机的速度,I mk 为电流分量的幅值,μ k 为电流分量的谐波次数,θ k 为电流分量的相位角。 v is the speed of the measured motor, I mk is the amplitude of the current component, μ k is the harmonic order of the current component, and θ k is the phase angle of the current component.

  (4)对电流滞环矢量控制系统注入三相谐波电流

Figure 14538DEST_PATH_IMAGE009
,对永磁型直线电机的推力波动进行抑制。  (4) Inject three-phase harmonic current into the current hysteresis vector control system
Figure 14538DEST_PATH_IMAGE009
, to suppress the thrust fluctuation of the permanent magnet linear motor.

本发明采用上述技术方案后具有以下有益效果: The present invention has following beneficial effect after adopting above-mentioned technical scheme:

1、本发明在普遍使用的电流滞环矢量控制驱动系统基础上,提出了注入电流谐波抵消初级永磁型直线电机定位力的控制方法,使得产生的附加电磁推力与定位力中的基波与主要高次谐波分量幅值相等、相位相反,可以相互抵消,从而达到抑制推力波动的目的,易于实现。 1. On the basis of the commonly used current hysteresis vector control drive system, the present invention proposes a control method for injecting current harmonics to offset the positioning force of the primary permanent magnet linear motor, so that the additional electromagnetic thrust generated and the fundamental wave in the positioning force The main high-order harmonic components are equal in amplitude and opposite in phase, and can cancel each other out, thereby achieving the purpose of suppressing thrust fluctuations, which is easy to implement.

2、本发明无需对电机本体进行改造,可以通过控制策略来实现,只需修改相关的控制软件,既可显著抑制电机推力波动,降低电机运行中的噪声,同时又保持了电机的空载磁势、推力输出能力等特性不变。 2. The present invention does not need to modify the motor body, and can be realized through the control strategy. It only needs to modify the relevant control software, which can significantly suppress the thrust fluctuation of the motor, reduce the noise during the operation of the motor, and maintain the no-load magnetic field of the motor at the same time. The characteristics such as potential and thrust output capability remain unchanged.

附图说明 Description of drawings

图1是初级永磁型直线电机的定位力波形; Figure 1 is the positioning force waveform of the primary permanent magnet linear motor;

图2是图1的定位力波形谐波分析; Fig. 2 is the positioning force waveform harmonic analysis of Fig. 1;

图3是初级永磁型直线电机的空载反电势波形; Figure 3 is the no-load back EMF waveform of the primary permanent magnet linear motor;

图4是本发明采用电流滞环矢量控制的用于抑制初级永磁型直线电机推力波动的控制系统框图; Fig. 4 is the control system block diagram that the present invention adopts current hysteresis vector control to suppress the thrust fluctuation of primary permanent magnet type linear motor;

图5是图4控制系统在谐波电流注入前的推力和电流波形; Figure 5 is the thrust and current waveforms of the control system in Figure 4 before harmonic current injection;

图6是图4控制系统在谐波电流注入后的推力和电流波形。 Figure 6 is the thrust and current waveforms of the control system in Figure 4 after harmonic current injection.

具体实施方式 Detailed ways

本发明基于常规的电流滞环矢量控制的初级永磁型直线电机驱动控制系统。首先,通过有限元仿真或转矩测试仪实测得到初级永磁型直线电机的定位力数据,利用傅里叶级数逼近法对定位力波形进行谐波频谱分析,确定定位力中k次基波与主要高次谐波分量,主要高次谐波分量的确定标准是将谐波分量幅值与基波幅值相比,比值较大而不能忽略的谐波分量确定为主要高次谐波分量。初级永磁型直线电机的定位力

Figure 891227DEST_PATH_IMAGE011
A k 为定位力的k次基波与主要高次谐波分量的幅值,φ k k次基波与主要高次谐波分量的相位角,
Figure 713690DEST_PATH_IMAGE002
τ s 为电机初级动子极距,x是初级动子位移。 The present invention is based on a conventional current hysteresis vector control primary permanent magnet linear motor drive control system. Firstly, the positioning force data of the primary permanent magnet linear motor is obtained through the finite element simulation or the actual measurement of the torque tester, and the harmonic spectrum analysis is performed on the positioning force waveform by using the Fourier series approximation method to determine the kth fundamental wave in the positioning force Compared with the main high-order harmonic component, the determination standard of the main high-order harmonic component is to compare the amplitude of the harmonic component with the amplitude of the fundamental wave, and the harmonic component whose ratio is large and cannot be ignored is determined as the main high-order harmonic component . Positioning Force of Primary Permanent Magnet Linear Motor ,
Figure 891227DEST_PATH_IMAGE011
, A k is the amplitude of the k -order fundamental wave and the main higher-order harmonic component of the positioning force, φ k is the phase angle between the k -order fundamental wave and the main higher-order harmonic component,
Figure 713690DEST_PATH_IMAGE002
, τ s is the pole distance of the primary mover of the motor, and x is the displacement of the primary mover.

其次,采用有限元仿真初级永磁型直线电机的空载反电势波形,对初级永磁型直线电机的反电势波形进行分析,写出相应的空载反电势数学表达式,空载反电势

Figure DEST_PATH_IMAGE012
E m 为反电势幅值。 Secondly, the no-load back EMF waveform of the primary permanent magnet linear motor is simulated by finite element analysis, the back EMF waveform of the primary permanent magnet linear motor is analyzed, and the corresponding no-load back EMF mathematical expression is written, the no-load back EMF
Figure DEST_PATH_IMAGE012
, Em is the magnitude of the back EMF.

初级永磁型直线电机的空载反电势波形呈正弦分布,除空载反电势的基波外,其余反电势的谐波含量忽略不计。 The no-load back EMF waveform of the primary permanent magnet linear motor is sinusoidally distributed, except for the fundamental wave of the no-load back EMF, the harmonic content of the rest of the back EMF is negligible.

然后,根据谐波电流分量与永磁反电势基波分量相互耦合,产生附加电磁推力分量的机理,计算得到相应的谐波电流分量,使得产生的附加电磁推力与定位力中的基波与主要高次谐波分量幅值相等、相位相反,即该附加电磁推力分量与定位力可大致相互抵消,可以相互抵消,从而达到抑制推力波动的目的。 Then, according to the mutual coupling between the harmonic current component and the fundamental wave component of the permanent magnet back EMF to generate an additional electromagnetic thrust component, the corresponding harmonic current component is calculated, so that the fundamental wave in the additional electromagnetic thrust and the positioning force is the same as the main The higher harmonic components have equal amplitudes and opposite phases, that is, the additional electromagnetic thrust component and the positioning force can roughly cancel each other out, so as to achieve the purpose of suppressing thrust fluctuations.

附加电磁推力

Figure 292307DEST_PATH_IMAGE013
v为实测电机的速度,
Figure 553524DEST_PATH_IMAGE015
Figure DEST_PATH_IMAGE016
是用于抵消k次定位力谐波分量的三相电流分量。 Additional Electromagnetic Thrust
Figure 292307DEST_PATH_IMAGE013
, v is the speed of the measured motor, ,
Figure 553524DEST_PATH_IMAGE015
,
Figure DEST_PATH_IMAGE016
is the three-phase current component used to offset the harmonic component of the k -order positioning force.

附加电磁推力F′ PMk 与定位力中的基波与主要高次谐波分量的幅值相等且相位相反,即有

Figure 35453DEST_PATH_IMAGE017
Figure 28816DEST_PATH_IMAGE006
Figure DEST_PATH_IMAGE018
,可以计算出用于抵消k次定位力谐波分量的三相电流分量
Figure 845463DEST_PATH_IMAGE014
 : The amplitude of the additional electromagnetic thrust F′ PMk and the fundamental wave in the positioning force and the main high-order harmonic components are equal and opposite in phase, that is,
Figure 35453DEST_PATH_IMAGE017
Figure 28816DEST_PATH_IMAGE006
Figure DEST_PATH_IMAGE018
, the three-phase current component used to offset the harmonic component of the k -order positioning force can be calculated
Figure 845463DEST_PATH_IMAGE014
, , :

Figure 909605DEST_PATH_IMAGE019
Figure 909605DEST_PATH_IMAGE019
,

I mk 为电流分量的幅值,μ k 为电流分量的谐波次数,θ k 为电流分量的相位角。 I mk is the magnitude of the current component, μ k is the harmonic order of the current component, and θ k is the phase angle of the current component.

     对电流滞环矢量控制系统注入三相谐波电流,抵消定位力,对永磁型直线电机的推力波动进行抑制。  Injecting three-phase harmonic current into current hysteresis vector control system , offset the positioning force, and suppress the thrust fluctuation of the permanent magnet linear motor.

以下以一台三相磁通切换初级永磁型直线电机为例进一步描述本发明。 The present invention will be further described below by taking a three-phase magnetic flux switching primary permanent magnet linear motor as an example.

实施例 Example

图1为采用有限元仿真得到的三相磁通切换初级永磁型直线电机的定位力波形。由图1可以看出,该三相磁通切换初级永磁型直线电机的定位力幅值较大,其波动峰-峰值超过330N,定位力波形包含有高次谐波分量,需要对其进行谐波分析以建立定位力的数学表达式,分析结果如图2所示。 Figure 1 is the positioning force waveform of the three-phase flux switching primary permanent magnet linear motor obtained by finite element simulation. It can be seen from Figure 1 that the positioning force amplitude of the three-phase flux switching primary permanent magnet linear motor is relatively large, and its peak-to-peak fluctuation exceeds 330N. The positioning force waveform contains high-order harmonic components, which need to be analyzed. Harmonic analysis is used to establish the mathematical expression of the positioning force, and the analysis results are shown in Figure 2.

下表1给出了定位力谐波分析的结果: Table 1 below presents the results of the positioning force harmonic analysis:

表1 定位力谐波分析 Table 1 Harmonic analysis of positioning force

 

Figure DEST_PATH_IMAGE020
 
Figure DEST_PATH_IMAGE020

由表1中的主要谐波分量的幅值、与基波分量的比值和相位角可见,定位力的谐波分量很大,其中2、5、6次谐波的幅值较大,与基波幅值比分别达到了15.45%、9.78%、13.75%,而剩下的其余高次谐波与基波的幅值比均小于5%,因此可以认为2、5、6次谐波为主要高次谐波分量,其余高次谐波可以忽略不计。这里的主要高次谐波分量是指谐波分量幅值与基波幅值相比较大而不能忽略的主要高次谐波分量。 It can be seen from the amplitude of the main harmonic components in Table 1, the ratio to the fundamental component and the phase angle, the harmonic components of the positioning force are very large, and the amplitudes of the 2nd, 5th and 6th harmonics are relatively large, which are different from the fundamental The wave amplitude ratios reached 15.45%, 9.78%, and 13.75% respectively, while the amplitude ratios of the remaining high-order harmonics to the fundamental wave were all less than 5%, so it can be considered that the 2nd, 5th, and 6th harmonics are the main Higher harmonic components, the rest of the higher harmonics can be ignored. The main high-order harmonic component here refers to the main high-order harmonic component whose amplitude is larger than that of the fundamental wave and cannot be ignored.

因此,磁通切换初级永磁型直线电机的定位力可以近似表达为: Therefore, the positioning force of the flux switching primary permanent magnet linear motor can be approximately expressed as:

Figure DEST_PATH_IMAGE021
                                          (1)
Figure DEST_PATH_IMAGE021
(1)

其中,τ s 为动子极距,A k φ k 分别为k次谐波分量的幅值和相位角,x是动子相对初始位置产生的位移。 Among them, τ s is the pole distance of the mover, A k and φ k are the amplitude and phase angle of the k -order harmonic component, and x is the displacement of the mover relative to the initial position.

图3为采用有限元仿真得到的空载反电势波形,利用wavestar软件对其进行谐波分析,可得到其总谐波畸变率(THD)仅为2.914%,谐波分量很小,因此空载反电势的数学表达式可表示为: Figure 3 is the no-load back EMF waveform obtained by finite element simulation. Using wavestar software to analyze its harmonics, it can be obtained that its total harmonic distortion (THD) is only 2.914%, and the harmonic components are very small, so no-load The mathematical expression of back EMF can be expressed as:

Figure DEST_PATH_IMAGE022
                                               (2)
Figure DEST_PATH_IMAGE022
(2)

其中E m 为反电势幅值。 Where E m is the magnitude of the back EMF.

根据谐波电流分量与永磁磁势基波分量相互耦合,产生附加电磁推力分量的机理,计算得到相应的谐波电流分量,使得产生的附加电磁推力与定位力中的基波与主要高次谐波分量幅值相等、相位相反,可以相互抵消,从而达到抑制推力波动的目的。具体如下: According to the mutual coupling between the harmonic current component and the fundamental wave component of the permanent magnet magnetic potential to generate additional electromagnetic thrust components, the corresponding harmonic current components are calculated, so that the fundamental wave and main high-order components in the additional electromagnetic thrust and positioning force generated The harmonic components have equal amplitudes and opposite phases, and can cancel each other out, thereby achieving the purpose of suppressing thrust fluctuations. details as follows:

用于抵消k次定位力谐波分量的附加电磁推力F′ PMk :  The additional electromagnetic thrust F′ PMk used to offset the harmonic component of the positioning force k times:

                                     (3) (3)

其中,F′ PMk 为用于抵消k次定位力谐波分量的附加电磁推力,i ak (x),i bk (x)i ck (x)为用于抵消k次定位力谐波分量的三相电流分量,v为实测电机的速度用于抵消k次定位力谐波分量的三相电流分量i ak (x)i bk (x)i ck (x)为: Among them, F′ PMk is the additional electromagnetic thrust used to cancel the harmonic component of the k -order positioning force, i ak (x) , i bk (x) and ick (x) are the additional electromagnetic thrust used to cancel the harmonic component of the k -order positioning force The three-phase current components, v is the speed of the measured motor , and the three-phase current components i ak (x) , i bk (x) and i ck (x) used to offset the harmonic component of the k -order positioning force are:

Figure 301721DEST_PATH_IMAGE019
                                          (4)
Figure 301721DEST_PATH_IMAGE019
(4)

其中,I mk 为电流分量的幅值,μ k 为电流分量的谐波次数,θ k 为电流分量的相位角。 Among them, I mk is the amplitude of the current component, μ k is the harmonic order of the current component, and θ k is the phase angle of the current component.

将公式(2)、(4)代入公式(3)可得: Substituting formula (2) and (4) into formula (3) can get:

Figure DEST_PATH_IMAGE024
                                   (5)
Figure DEST_PATH_IMAGE024
(5)

因此三相注入谐波电流可表达为: Therefore, the three-phase injected harmonic current can be expressed as:

Figure 280214DEST_PATH_IMAGE025
                                                      (6)
Figure 280214DEST_PATH_IMAGE025
(6)

对电流滞环矢量控制系统注入所述三相谐波电流可对永磁型直线电机的推力波动进行抑制。 Injecting the three-phase harmonic current into the current hysteresis vector control system can suppress the thrust fluctuation of the permanent magnet linear motor.

以下提供本发明的仿真应用例,由此可得知本发明的效果: The simulation application example of the present invention is provided below, thus can know effect of the present invention:

如图4所示,在电流滞环矢量控制的磁通切换永磁直线电机驱动系统基础上,结合上述的谐波电流注入法,可得到如图4的相应的抑制磁通切换的初级永磁型直线电机推力波动的控制系统,该控制系统包括PI转速调节器1、推力-电流变换模块2、2r/3s变换(转子旋转两相/定子静止三相变换)模块3、求和模块4、电流滞环PWM模块5、逆变器6、LFSPM电机7(初级永磁型直线电机7)、光电编码器8、电机速度与位置检测模块9、谐波电流求解模块10。根据实测电机的速度v和指定速度v * ,求出速度差v(n);该速度差通过PI转速调节器1,得到所需的电磁推力指令值F e * ;采用I d =0控制,通过推力-电流变换模块2,由F e * 得到对应的交直轴电流参考值i d * i q * ;利用反馈的动子位置角θ e ,经模块3做2r/3s变换,得到定子静止坐标系下的三相绕组电流i a i b i c ;该电流与由谐波电流求解模块10求得的谐波电流i a i b i c 一起通过求和模块4计算,得到所需的三相绕组电流参考值i a * i b * i c * ;该参考电流i a * i b * i c * 与三相绕组实时电流反馈值i a1 i b1 i c1 经过电流滞环PWM模块5进行滞环比较,得到逆变器6中电力电子器件的PWM导通关断信号,从而控制绕组中的电流跟随指令电流值;通过光电编码器8测得LFSPM电机7的脉冲信号,再通过电机速度与位置检测模块9计算出电机的实时反馈速度v和动子位置角θ e ,用于速度环的闭环控制和相应的计算。根据图4的框图建立Matlab/Simulink仿真模型。图5为谐波电流注入前的推力和电流波形,图6为谐波电流注入后的推力和电流波形。由图5和图6可以看出:谐波电流注入前推力脉动峰-峰值达到386N,每相电流呈现良好的正弦性;谐波电流注入后推力脉动峰-峰值只有165N,而每相电流包含一定的谐波成分,该谐波成分产生的电磁推力正好抵消磁通切换永磁直线电机的定位力。仿真结果证明本发明提出的控制策略显著抑制了初级永磁型电机的推力波动,同时又保持了电机的推力输出能力不变。 As shown in Figure 4, on the basis of the magnetic flux switching permanent magnet linear motor drive system controlled by the current hysteresis vector control, combined with the above-mentioned harmonic current injection method, the corresponding primary permanent magnet that inhibits magnetic flux switching can be obtained as shown in Figure 4 Type linear motor thrust fluctuation control system, the control system includes PI speed regulator 1, thrust-current conversion module 2, 2r/3s conversion (rotor rotating two-phase/stator stationary three-phase conversion) module 3, summation module 4, Current hysteresis PWM module 5, inverter 6, LFSPM motor 7 (primary permanent magnet linear motor 7), photoelectric encoder 8, motor speed and position detection module 9, harmonic current solution module 10. According to the speed v of the measured motor and the specified speed v * , the speed difference v(n) is obtained; the speed difference is passed through the PI speed regulator 1 to obtain the required electromagnetic thrust command value F e * ; using I d =0 control, Through the thrust-current conversion module 2, the corresponding reference values of the orthogonal and direct axis currents i d * and i q * are obtained from F e * ; using the feedback position angle θ e of the mover, the 2r/3s transformation is performed through the module 3 to obtain the static state of the stator The three-phase winding currents ia , ib , ic in the coordinate system; this current, together with the harmonic currents ia ' , ib ' , ic ' obtained by the harmonic current solution module 10 , passes through the summation module 4 Calculate and obtain the required three-phase winding current reference value i a * , i b * , i c * ; the reference current i a * , i b * , i c * and the three-phase winding real-time current feedback value i a1 , i b1 and i c1 go through the current hysteresis PWM module 5 for hysteresis comparison, and get the PWM on-off signal of the power electronic device in the inverter 6, so as to control the current in the winding to follow the command current value; Obtain the pulse signal of the LFSPM motor 7, and then calculate the real-time feedback speed v of the motor and the mover position angle θ e through the motor speed and position detection module 9, which are used for the closed-loop control of the speed loop and corresponding calculations. Establish the Matlab/Simulink simulation model according to the block diagram in Figure 4. Figure 5 shows the thrust and current waveforms before harmonic current injection, and Figure 6 shows the thrust and current waveforms after harmonic current injection. It can be seen from Figure 5 and Figure 6 that: before the harmonic current injection, the peak-to-peak value of the thrust pulsation reaches 386N, and the current of each phase presents a good sinusoid; A certain harmonic component, the electromagnetic thrust generated by the harmonic component just offsets the positioning force of the flux switching permanent magnet linear motor. The simulation results prove that the control strategy proposed by the present invention significantly suppresses the thrust fluctuation of the primary permanent magnet motor, while keeping the thrust output capability of the motor unchanged.

Claims (1)

1. the force oscillation inhibition method of a primary permanent magnet type linear motor adopts conventional current hysteresis ring vector control system, it is characterized in that may further comprise the steps:
(1) surveys the detent force that obtains primary permanent magnet type linear motor by finite element simulation or torque tester
Figure 2013102440270100001DEST_PATH_IMAGE001
, utilize the Fourier series approximatioss that the waveform of detent force is carried out the harmonic spectrum analysis, determine first-harmonic and main higher harmonic components in the detent force; A k For kThe amplitude of inferior detent force harmonic component, φ k For kThe phase angle of inferior detent force harmonic component,
Figure 521803DEST_PATH_IMAGE002
, τ s Be electric motor primary mover pole span, xIt is elementary mover displacement;
(2) the unloaded counter potential waveform of employing finite element simulation primary permanent magnet type linear motor is determined unloaded back-emf , E m Be the back-emf amplitude;
(3) according to additional electromagnetic thrust And additional electromagnetic thrust F ' PMk Equate with the amplitude of main higher harmonic components with first-harmonic in the detent force and phase place opposite,
Figure 548851DEST_PATH_IMAGE006
, calculate for counteracting kThe three-phase current component of inferior detent force harmonic component i Ak (x), i Bk (x), i Ck (x):
Figure 917515DEST_PATH_IMAGE008
vBe the speed of actual measurement motor, I Mk Be the amplitude of current component, μ k Be the harmonic number of current component, θ k Phase angle for current component;
(4) current hysteresis ring vector control system is injected the three phase harmonic electric current
Figure DEST_PATH_IMAGE009
, the force oscillation of permanent magnet type linear motor is suppressed.
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Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN107395091A (en) * 2017-07-24 2017-11-24 东南大学 A kind of linear induction motor system detent force cutting method
CN109889110A (en) * 2019-03-14 2019-06-14 西北工业大学 A multi-stage starter/generator starting torque calculation method
CN112234893A (en) * 2020-09-21 2021-01-15 瑞声新能源发展(常州)有限公司科教城分公司 Method for suppressing thrust fluctuation of linear motor, related equipment and medium
CN112234891A (en) * 2020-09-21 2021-01-15 瑞声新能源发展(常州)有限公司科教城分公司 Method for suppressing thrust fluctuation of linear motor, related equipment and medium
CN112234892A (en) * 2020-09-21 2021-01-15 瑞声新能源发展(常州)有限公司科教城分公司 Method for suppressing thrust fluctuation of linear motor, related equipment and medium
CN114759859A (en) * 2022-05-18 2022-07-15 哈尔滨工业大学 Thrust fluctuation fitting method for segmented linear motor
CN117526813A (en) * 2023-11-09 2024-02-06 中国矿业大学 Optimization method of electromagnetic force of motor

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004032944A (en) * 2002-06-27 2004-01-29 Okuma Corp Control device for synchronous motor and synchronous motor
CN101515780A (en) * 2009-04-03 2009-08-26 东南大学 Control method for compensating location torque of permanent-magnet motor by injecting current harmonics
CN102931907A (en) * 2012-11-15 2013-02-13 上海海事大学 Energy-saving transportation system based on permanent-magnet linear motor

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2004032944A (en) * 2002-06-27 2004-01-29 Okuma Corp Control device for synchronous motor and synchronous motor
CN101515780A (en) * 2009-04-03 2009-08-26 东南大学 Control method for compensating location torque of permanent-magnet motor by injecting current harmonics
CN102931907A (en) * 2012-11-15 2013-02-13 上海海事大学 Energy-saving transportation system based on permanent-magnet linear motor

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* Cited by examiner, † Cited by third party
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CN109889110B (en) * 2019-03-14 2020-09-22 西北工业大学 Method for calculating starting torque of multi-stage starting/power generator
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CN112234892A (en) * 2020-09-21 2021-01-15 瑞声新能源发展(常州)有限公司科教城分公司 Method for suppressing thrust fluctuation of linear motor, related equipment and medium
WO2022056976A1 (en) * 2020-09-21 2022-03-24 瑞声声学科技(深圳)有限公司 Method for restraining thrust ripple of linear motor, related device, and medium
WO2022057010A1 (en) * 2020-09-21 2022-03-24 瑞声声学科技(深圳)有限公司 Method for suppressing thrust ripple of linear motor, related device, and medium
WO2022056981A1 (en) * 2020-09-21 2022-03-24 瑞声声学科技(深圳)有限公司 Method for suppressing thrust ripple of linear motor, and related device and medium
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