Deprecated: The each() function is deprecated. This message will be suppressed on further calls in /home/zhenxiangba/zhenxiangba.com/public_html/phproxy-improved-master/index.php on line 456
JP3566577B2 - Induction motor control device - Google Patents
[go: Go Back, main page]

JP3566577B2 - Induction motor control device - Google Patents

Induction motor control device Download PDF

Info

Publication number
JP3566577B2
JP3566577B2 JP09078499A JP9078499A JP3566577B2 JP 3566577 B2 JP3566577 B2 JP 3566577B2 JP 09078499 A JP09078499 A JP 09078499A JP 9078499 A JP9078499 A JP 9078499A JP 3566577 B2 JP3566577 B2 JP 3566577B2
Authority
JP
Japan
Prior art keywords
magnetic flux
estimating means
speed estimating
induction motor
speed
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
JP09078499A
Other languages
Japanese (ja)
Other versions
JP2000287491A (en
Inventor
洋一 大森
知明 桐谷
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Toyo Electric Manufacturing Ltd
Original Assignee
Toyo Electric Manufacturing Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Toyo Electric Manufacturing Ltd filed Critical Toyo Electric Manufacturing Ltd
Priority to JP09078499A priority Critical patent/JP3566577B2/en
Publication of JP2000287491A publication Critical patent/JP2000287491A/en
Application granted granted Critical
Publication of JP3566577B2 publication Critical patent/JP3566577B2/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Landscapes

  • Motor And Converter Starters (AREA)
  • Control Of Electric Motors In General (AREA)
  • Control Of Ac Motors In General (AREA)

Description

【0001】
【発明の属する技術分野】
本発明は,交流電動機を駆動するインバータの制御に関するもので,特に始動を滑らかにするものである。
【0002】
【従来の技術】
従来の技術の1例を図2に示し,図2に基づいて従来の技術を説明する。
通常運転状態では,運転切換器7は通常運転制御器5を選択して,通常運転制御器5の出力の制御信号を電力変換器1に入力する。電力変換器1は入力した制御信号に基づいて誘導電動機4に電力を供給する。
【0003】
誘導電動機4に電力を供給し始めた直後の所定の微少期間t1は,運転切換器7は第1速度推定手段8を選択する。第1速度推定手段8は,誘導電動機4の入力電流が零または零に近い値の直流電流となるような制御信号を出力して,磁束演算手段6の出力の磁束ベクトルを入力して,前記微少期間t1の磁束ベクトルの軌跡である円弧の中心を求めて,円弧の中心角θを得て
ω0=θ/t1 ▲1▼
により誘導電動機4の回転角周波数ω0を求めて出力する。また第1速度推定手段8は,
φ0=f1−f0 ▲2▼
により誘導電動機4の残留磁束ベクトルφ0を求めて出力する。ここでf0は,円弧の中心の磁束ベクトルであり,f1は,前記微少期間t1の最終時点での磁束ベクトルである。
【0004】
誘導電動機4の回転角周波数ω0が0に近かったり,残留磁束が非常に小さい場合は,第1速度推定手段8において,磁束演算手段6の出力の磁束ベクトルは円弧状にならなかったり非常に小さな円弧になるので,回転角周波数ω0や残留磁束ベクトルφ0を求められない。その場合運転切換器7は,第1速度推定手段8を選択した後の所定の微少期間t2の間、第2速度推定手段9を選択する。第1速度推定手段8で回転角周波数ω0や残留磁束ベクトルφ0が求めることができた場合は運転切換器7は,通常運転制御器5を選択する。
【0005】
第2速度推定手段9は,前記誘導電動機の入力電流が所定の直流電流ベクトルix1となるようにして,第1速度推定手段8と同様に誘導電動機4の残留磁束ベクトルφ0を求めて出力する。また第2速度推定手段9は,

Figure 0003566577
により残留磁束ベクトルφ0を求めて出力する。ここで,T2は誘導電動機4の2次時定数,Mは相互インダクタンス,jは虚数単位,expは指数関数である。誘導電動機4の回転角周波数ω0が0に近い場合は,第2速度推定手段9においても磁束演算手段6の出力の磁束ベクトルが円弧状にならないので,ω0を求めることができないが,その場合はω0=0およびφ0=0を出力する。
【0006】
運転切換器7は,第2速度推定手段9を選択した後は,通常運転制御器5を選択する。通常運転制御器5は,第1速度推定手段8または第2速度推定手段9で求められた誘導電動機4の回転角周波数ω0や残留磁束ベクトルφ0を回転角周波数や磁束の演算の初期値として使用して,誘導電動機4が所定の出力トルクや所定の速度状態となるような制御信号を出力する。
【0007】
【発明が解決しようとする課題】
第1の問題を以下に示す。誘導電動機に直流電流ベクトルixを流した時の磁束ベクトルφは,
φ=φx+(φx0−φx)・exp(j・ω0・t−t/T2) ▲4▼
で表される。ここでtは経過時間,φx0は直流電流ベクトルixを流し始めたときの磁束,φxは
φx=M・ix/(1−j・ω0・T2) ▲5▼
である。▲4▼式より磁束ベクトルφは,半径φx0−φxの円弧を描き,その中心はφxとなることが分かる。
【0008】
従来の技術において,誘導電動機が回転している場合,第2速度推定手段9では回転角周波数ω0を求めることができるとしている。しかし,▲4▼式のφx0−φxが零に近い値の場合では,磁束ベクトルφの描く円の半径が非常に小さいことになり,その円の回転角を求めることができず,回転角周波数ω0を求めることができなくなる。すると第2速度推定手段9では,ω0=0として出力するので,通常運転制御器5においてω0は0でないにも関わらずω0=0として制御をすることになり,正常な制御ができなくなる。
【0009】
第2の問題を以下に示す。誘導電動機が回転している場合,第1速度推定手段8や第2速度推定手段9で用いる磁束演算手段6の出力の磁束ベクトルは円弧を描くとしているが,例えば誘導電動機の回転子のスロットがスキューされてないことにより空間高調波が大きい誘導電動機では,磁束ベクトルは前記空間高調波によって発生する高調波成分を含むようになり,磁束演算手段6の出力の磁束ベクトルは円弧に高調波が重畳されたようになる。すると円弧の中心および中心角を求める際の誤差が大きくなり,それによって求められる回転角周波数ω0や残留磁束ベクトルφ0に誤差を含むようになる。
【0010】
第3の問題を以下に示す。第2速度推定手段9において,残留磁束ベクトルφ0を▲3▼式によって求めているが,これは▲4▼式からφx0=0として導き出された式である。よって第2速度推定手段を開始した時に磁束が残っていてφx0が0でない場合は,残留磁束ベクトルφ0の計算を間違えてしまう。
【0011】
第4の問題を以下に示す。第1速度推定手段8の微少時間t1や第2速度推定手段9の微少時間t2が固定値の場合,磁束ベクトルの円弧の中心角θは回転角周波数ω0に比例して広がる。するとω0が非常に大きな場合は,θは180度を越えてしまうことがあり,最初の時点の磁束ベクトルと最後の時点の磁束ベクトルと円弧の中心の情報より中心角を求めている場合は,θの計算を間違う恐れがある。
本発明は上述した点に鑑みて創案されたもので、その目的とするところは、これらの課題を解消し、始動時における誘導電動機の回転角周波数や残留磁束ベクトルがより正確により確実に把握でき,通常運転制御におけるトルクや速度の制御への移行時に,過電流になったり急加減速などの過渡現象が生じなくなる誘導電動機の制御装置を提供することにある。
【0012】
【課題を解決するための手段】
つまり、その目的を達成するための手段は、
1.請求項1において、
前記第1の問題を解決するために,第2速度推定手段で速度が推定できなかった場合で,該第2速度推定手段の実行直後に,前記第2速度推定手段で流した電流と逆方向に直流電流を流すようにして他は前記第2速度推定手段と同じ方法で前記誘導電動機の回転角周波数と残留磁束ベクトルを推定する第3速度推定手段を具備する。
【0013】
2.請求項2において、
前記第2の問題を解決するために,前記第1,第2または第3の速度推定手段において,前記磁束演算手段の出力の磁束ベクトルの軌跡である円弧の中心を求める際に,円弧の最初から最後までの時間を3等分して,それぞれの時間領域における円弧の平均値を計算して3点を求めて,該3点を通る円の中心を求めて前記円弧の中心とすることを特徴とする。
【0014】
3.請求項3において、
前記第3の問題を解決するために,前記第2または第3速度推定手段において,該第2または第3速度推定手段で流す直流電流ベクトルをixとし,該第2または第3速度推定手段で得られた速度に相当する角周波数をω0とし,前記誘導電動機の2次時定数をT2,相互インダクタンスをMとし,虚数単位をjで表して,前記磁束演算手段の出力の磁束ベクトルの軌跡である円弧の中心のベクトルをf0とし,前記第2または第3速度推定手段の最後の時点での前記磁束演算手段の出力の磁束ベクトルをf1として,残留磁束ベクトルφ0を,
φ0=M・ix/(1−j・ω0・T2)+f1−f0 ▲6▼
により求める第2または第3速度推定手段を具備する。
【0015】
4.請求項4において、
前記第4の問題を解決するために,前記第1速度推定手段の微少時間t1,および前記第2または第3速度推定手段の微少時間t2を,所定の最大時間と,前記磁束演算手段の出力の磁束ベクトルの軌跡である円弧の中心角が所定の角度になる時間との短い方の時間とすることを特徴とする。
以下、本発明の一実施例を図面に基づいて詳述する。
【0016】
【発明の実施の形態】
本発明の実施例を図1のブロック図に示し,図1に基づいて説明する。なお、符号1〜9の説明は,従来技術で説明したので省く。
第2速度推定手段9において,回転角周波数ω0を求めることができなかった場合は,運転切換器7は,第2速度推定手段9を選択した後の所定の微少期間t2の間,第3速度推定手段10を選択する。
第3速度推定手段10は,前記誘導電動機の入力電流が所定の直流電流ベクトルix2となるようにして,第2速度推定手段9と同様に,誘導電動機4の回転角周波数ω0と残留磁束ベクトルφ0を求めて出力する。この場合流す直流電流ベクトルの向きは第2速度推定手段9の場合の逆とする。
つまりix2=−ix1の関係とする。第2速度推定手段9で回転角周波数を求めることができないのは,回転が停止している場合か▲4▼式のφx0−φxが零に近い値の場合のどちらかである。第3速度推定手段10においては,ix2=−ix1とすることにより,後者の場合を除くことができるので,回転角周波数を間違いなく求めることが可能となる。
【0017】
本実施例の第2速度推定手段9や第3速度推定手段10において,残留磁束ベクトルφ0は,▲3▼式の代わりに▲6▼式で求められる。ここで▲6▼式のixには,第2速度推定手段9の場合ix1を適用し,第3速度推定手段10の場合ix2を適用する。▲6▼式の第1項は▲4▼式の第1項を表しており,▲6▼式のf1−f0の項は▲4▼式の第2項のt=t2に相当するため,第2または第3速度推定手段を開始した時に磁束が残っていてφx0が0でなくても,▲6▼式では正確に残留磁束ベクトルφ0を求めることができる。
【0018】
本実施例の第1速度推定手段8や第2速度推定手段9や第3速度推定手段10の磁束ベクトル軌跡の円弧の中心を求める方法を図3に基づいて説明する。
微少期間t1またはt2を3等分してそれらを時間順に期間ta,tb,tcとする。期間taでの磁束軌跡の平均点をPaとし,他の2つの期間の磁束軌跡の平均点をそれぞれPb,Pcとして求める。これらPa,Pb,Pcの3点を通る円の中心を求める。Pa点からPc点までの円弧の中心角θxを求め,それを1.5倍して▲1▼式で用いるθとする。
【0019】
本実施例の第1速度推定手段8の微少期間t1および第2速度推定手段9や第3速度推定手段10の微少期間t2は,磁束演算手段6の出力の磁束ベクトルの軌跡である円弧の中心角が所定の角度例えば180度を越える時間とする。
つまり各速度推定手段において随時中心角を求めておき,その中心角が例えば180度を越えた時点で回転角周波数ω0や残留磁束ベクトルφ0を求めて,各速度推定手段を終了するようにする。なお円弧の中心角が所定の角度を越えていない場でも所定時間例えば20msecを経過していれば,回転角周波数ω0や残留磁束ベクトルφ0を求めて,各速度推定手段を終了するようにする。
【0020】
【発明の効果】
以上述べたように本発明によれば,始動時における誘導電動機の回転角周波数や残留磁束ベクトルがより正確により確実に把握できるため,通常運転制御におけるトルクや速度の制御への移行時に,過電流になったり急加減速などの過渡現象が生じなくなり,実用上、極めて有用性の高いものである。
【図面の簡単な説明】
【図1】本発明の1実施例を表すブロック図である。
【図2】従来の1例を表すブロック図である。
【図3】速度推定手段での磁束ベクトル軌跡の1例である。
【符号の説明】
1 電力変換器
2 電流ベクトル検出器
3 電圧ベクトル検出器
4 誘導電動機
5 通常運転制御器
6 磁束演算手段
7 運転切替器
8 第1速度推定手段
9 第2速度推定手段
10 第3速度推定手段[0001]
TECHNICAL FIELD OF THE INVENTION
The present invention relates to control of an inverter that drives an AC motor, and particularly to smooth starting.
[0002]
[Prior art]
FIG. 2 shows an example of the conventional technique, and the conventional technique will be described with reference to FIG.
In the normal operation state, the operation switching unit 7 selects the normal operation controller 5 and inputs a control signal output from the normal operation controller 5 to the power converter 1. The power converter 1 supplies power to the induction motor 4 based on the input control signal.
[0003]
During a predetermined minute period t1 immediately after the power supply to the induction motor 4 is started, the operation switch 7 selects the first speed estimating means 8. The first speed estimating means 8 outputs a control signal such that the input current of the induction motor 4 becomes a DC current of zero or a value close to zero, inputs the magnetic flux vector of the output of the magnetic flux calculating means 6, and The center of the arc which is the trajectory of the magnetic flux vector in the minute period t1 is obtained, and the center angle θ of the arc is obtained to obtain ω0 = θ / t1 (1)
To obtain and output the rotational angular frequency ω0 of the induction motor 4. The first speed estimating means 8
φ0 = f1-f0 (2)
To obtain and output the residual magnetic flux vector φ0 of the induction motor 4. Here, f0 is a magnetic flux vector at the center of the arc, and f1 is a magnetic flux vector at the end of the minute period t1.
[0004]
When the rotational angular frequency ω0 of the induction motor 4 is close to 0 or the residual magnetic flux is very small, the first speed estimating means 8 does not make the magnetic flux vector output from the magnetic flux calculating means 6 circular or very small. Since it is a circular arc, the rotational angular frequency ω0 and the residual magnetic flux vector φ0 cannot be obtained. In that case, the operation switching device 7 selects the second speed estimating means 9 for a predetermined minute period t2 after selecting the first speed estimating means 8. When the rotation speed ω0 and the residual magnetic flux vector φ0 can be obtained by the first speed estimating means 8, the operation switching unit 7 selects the normal operation controller 5.
[0005]
The second speed estimating means 9 calculates and outputs the residual magnetic flux vector φ0 of the induction motor 4 in the same manner as the first speed estimating means 8 so that the input current of the induction motor becomes a predetermined DC current vector ix1. The second speed estimating means 9
Figure 0003566577
To obtain and output the residual magnetic flux vector φ0. Here, T2 is a secondary time constant of the induction motor 4, M is a mutual inductance, j is an imaginary unit, and exp is an exponential function. If the rotational angular frequency ω0 of the induction motor 4 is close to 0, the second speed estimating means 9 cannot obtain ω0 because the magnetic flux vector output from the magnetic flux calculating means 6 does not have an arc shape. ω0 = 0 and φ0 = 0 are output.
[0006]
After selecting the second speed estimating means 9, the operation switching device 7 selects the normal operation controller 5. The normal operation controller 5 uses the rotation angular frequency ω0 and the residual magnetic flux vector φ0 of the induction motor 4 obtained by the first speed estimating means 8 or the second speed estimating means 9 as initial values for calculating the rotation angular frequency and the magnetic flux. Then, a control signal is output such that the induction motor 4 is set to a predetermined output torque or a predetermined speed state.
[0007]
[Problems to be solved by the invention]
The first problem is shown below. The magnetic flux vector φ when the DC current vector ix is passed through the induction motor is
φ = φx + (φx0−φx) · exp (j · ω0 · tt / T2) (4)
It is represented by Here, t is the elapsed time, φx0 is the magnetic flux when the DC current vector ix starts to flow, and φx is φx = M · ix / (1-j · ω0 · T2).
It is. From equation (4), it can be seen that the magnetic flux vector φ draws an arc with a radius φx0−φx, and the center is φx.
[0008]
According to the conventional technology, when the induction motor is rotating, the second speed estimating means 9 can determine the rotation angular frequency ω0. However, when φx0−φx in equation (4) is a value close to zero, the radius of the circle drawn by the magnetic flux vector φ is very small, and the rotation angle of the circle cannot be obtained, and the rotation angle frequency ω0 cannot be obtained. Then, since the second speed estimating means 9 outputs ω0 = 0, the normal operation controller 5 controls ω0 = 0 even though ω0 is not 0, and normal control cannot be performed.
[0009]
The second problem is described below. When the induction motor is rotating, the magnetic flux vector output from the magnetic flux calculating means 6 used in the first speed estimating means 8 and the second speed estimating means 9 is assumed to draw a circular arc. In an induction motor having large spatial harmonics because it is not skewed, the magnetic flux vector includes a harmonic component generated by the spatial harmonics, and the magnetic flux vector output from the magnetic flux calculating means 6 has the harmonics superimposed on an arc. It will be like. Then, an error in obtaining the center and the central angle of the arc increases, and the rotation angular frequency ω0 and the residual magnetic flux vector φ0 obtained by the error include errors.
[0010]
The third problem is described below. In the second velocity estimating means 9, the residual magnetic flux vector φ0 is obtained by the formula (3), which is derived from the formula (4) as φx0 = 0. Therefore, when the magnetic flux remains when the second speed estimating means is started and φx0 is not 0, the calculation of the residual magnetic flux vector φ0 is erroneously performed.
[0011]
The fourth problem is described below. When the minute time t1 of the first speed estimating means 8 and the minute time t2 of the second speed estimating means 9 are fixed values, the center angle θ of the arc of the magnetic flux vector spreads in proportion to the rotation angular frequency ω0. If ω0 is very large, θ may exceed 180 degrees. If the center angle is obtained from the information of the magnetic flux vector at the first time, the magnetic flux vector at the last time, and the center of the arc, The calculation of θ may be wrong.
The present invention has been made in view of the above points, and aims to solve these problems, and to more accurately and reliably grasp the rotational angular frequency and the residual magnetic flux vector of an induction motor at the time of starting. Another object of the present invention is to provide a control device for an induction motor in which transient phenomena such as overcurrent and rapid acceleration / deceleration do not occur when shifting to control of torque or speed in normal operation control.
[0012]
[Means for Solving the Problems]
In other words, the means to achieve that goal are:
1. In claim 1,
In order to solve the first problem, in the case where the speed cannot be estimated by the second speed estimating means, immediately after the execution of the second speed estimating means, the current flows in the opposite direction to the current flowing by the second speed estimating means. And a third speed estimating means for estimating a rotational angular frequency and a residual magnetic flux vector of the induction motor in the same manner as the second speed estimating means except that a direct current is supplied to the motor.
[0013]
2. In claim 2,
In order to solve the second problem, the first, second or third speed estimating means may determine the center of the arc which is the trajectory of the magnetic flux vector output from the magnetic flux calculating means. Dividing the time from the end to the end into three equal parts, calculating the average value of the arcs in the respective time domains, obtaining three points, obtaining the center of a circle passing through the three points, and setting the center of the arc as the center of the arc. Features.
[0014]
3. In claim 3,
In order to solve the third problem, in the second or third speed estimating means, the DC current vector flowing in the second or third speed estimating means is ix, and the second or third speed estimating means is ix. The angular frequency corresponding to the obtained speed is ω 0, the secondary time constant of the induction motor is T 2, the mutual inductance is M, the imaginary unit is j, and the trajectory of the magnetic flux vector output from the magnetic flux calculating means is Let f0 be the vector at the center of a certain arc, and let f1 be the magnetic flux vector output from the magnetic flux calculating means at the last point in time of the second or third speed estimating means.
φ0 = M · ix / (1−j · ω0 · T2) + f1−f0 (6)
And a second or third speed estimating means.
[0015]
4. In claim 4,
In order to solve the fourth problem, the minute time t1 of the first speed estimating means and the minute time t2 of the second or third speed estimating means are set to a predetermined maximum time and the output of the magnetic flux calculating means. And the time at which the center angle of the arc, which is the locus of the magnetic flux vector, becomes a predetermined angle, is the shorter time.
Hereinafter, an embodiment of the present invention will be described in detail with reference to the drawings.
[0016]
BEST MODE FOR CARRYING OUT THE INVENTION
An embodiment of the present invention is shown in the block diagram of FIG. 1 and will be described with reference to FIG. The description of reference numerals 1 to 9 is omitted because it has been described in the prior art.
If the second speed estimating means 9 cannot find the rotation angular frequency ω0, the operation switching device 7 sets the third speed estimating means 9 to the third speed during a predetermined minute period t2 after the second speed estimating means 9 is selected. The estimating means 10 is selected.
The third speed estimating means 10 controls the rotation angle frequency ω0 and the residual magnetic flux vector φ0 of the induction motor 4 in the same manner as the second speed estimating means 9 so that the input current of the induction motor becomes a predetermined DC current vector ix2. Is output. In this case, the direction of the direct current vector flowing is reverse to that of the second speed estimating means 9.
That is, a relationship of ix2 = −ix1 is set. The rotation speed cannot be determined by the second speed estimating means 9 either when the rotation is stopped or when φx0−φx in the equation (4) is a value close to zero. In the third speed estimating means 10, the latter case can be eliminated by setting ix2 = -ix1, so that the rotational angular frequency can be determined without fail.
[0017]
In the second speed estimating means 9 and the third speed estimating means 10 of the present embodiment, the residual magnetic flux vector φ0 is obtained by Expression (6) instead of Expression (3). Here, ix1 in the case of the second speed estimating means 9 and ix2 in the case of the third speed estimating means 10 are applied to ix in the equation (6). The first term of equation (6) represents the first term of equation (4), and the term f1-f0 of equation (6) corresponds to t = t2 of the second term of equation (4). Even if the magnetic flux remains when the second or third speed estimating means is started and φx0 is not 0, the residual magnetic flux vector φ0 can be accurately obtained by the equation (6).
[0018]
A method for obtaining the center of the arc of the magnetic flux vector locus of the first speed estimating means 8, the second speed estimating means 9, and the third speed estimating means 10 of this embodiment will be described with reference to FIG.
The minute period t1 or t2 is divided into three equal parts, and these are set as periods ta, tb, and tc in time order. The average point of the magnetic flux trajectory in the period ta is determined as Pa, and the average points of the magnetic flux trajectories in the other two periods are determined as Pb and Pc, respectively. The center of a circle passing through these three points Pa, Pb, and Pc is obtained. The center angle θx of the arc from the point Pa to the point Pc is obtained, multiplied by 1.5 and defined as θ used in the equation (1).
[0019]
In the present embodiment, the minute period t1 of the first speed estimating means 8 and the minute period t2 of the second speed estimating means 9 and the third speed estimating means 10 correspond to the center of the arc which is the locus of the magnetic flux vector output from the magnetic flux calculating means 6. Assume that the angle exceeds a predetermined angle, for example, 180 degrees.
In other words, the center angle is obtained as needed in each speed estimating means, and when the center angle exceeds 180 degrees, for example, the rotational angular frequency ω0 and the residual magnetic flux vector φ0 are obtained, and each speed estimating means is terminated. Even if the center angle of the circular arc does not exceed the predetermined angle, if the predetermined time, for example, 20 msec has elapsed, the rotational angular frequency ω0 and the residual magnetic flux vector φ0 are obtained, and each speed estimating means is terminated.
[0020]
【The invention's effect】
As described above, according to the present invention, the rotational angular frequency and the residual magnetic flux vector of the induction motor at the time of starting can be grasped more accurately and more reliably. No transient phenomena such as sudden acceleration or deceleration occur, which is extremely useful in practical use.
[Brief description of the drawings]
FIG. 1 is a block diagram showing one embodiment of the present invention.
FIG. 2 is a block diagram illustrating a conventional example.
FIG. 3 is an example of a magnetic flux vector locus in a speed estimating unit.
[Explanation of symbols]
DESCRIPTION OF SYMBOLS 1 Power converter 2 Current vector detector 3 Voltage vector detector 4 Induction motor 5 Normal operation controller 6 Magnetic flux calculation means 7 Operation switch 8 First speed estimation means 9 Second speed estimation means 10 Third speed estimation means

Claims (4)

誘導電動機の入力電圧ベクトルから一次抵抗と漏れインダクタンスによる電圧降下を除いたものを時間積分して磁束ベクトルを演算する磁束演算手段と,前記誘導電動機に電力を供給し始めた直後の所定の微少期間t1に,前記誘導電動機の入力電流が零または零に近い値の直流電流となるようにして,前記磁束演算手段の出力の磁束ベクトルの軌跡である円弧の中心を求めて前記誘導電動機の回転角周波数と残留磁束ベクトルを推定する第1速度推定手段と,前記第1速度推定手段で速度が推定できなかった場合で,該第1速度推定手段の実行直後の所定の微少期間t2に,前記誘導電動機の入力電流が所定の直流電流ベクトルとなるようにして,前記磁束演算手段の出力の磁束ベクトルの軌跡である円弧の中心を求めて前記誘導電動機の回転角周波数と残留磁束ベクトルを推定する第2速度推定手段とを具備した誘導電動機に電力を供給する電力変換器を制御する誘導電動機の制御装置において,
前記第2速度推定手段で速度が推定できなかった場合で,該第2速度推定手段の実行直後に,前記第2速度推定手段で流した電流と逆方向に直流電流を流すようにして他は前記第2速度推定手段と同じ方法で前記誘導電動機の回転角周波数と残留磁束ベクトルを推定する第3速度推定手段を具備することを特徴とする誘導電動機の制御装置。
Magnetic flux calculating means for calculating a magnetic flux vector by time-integrating a value obtained by removing a voltage drop due to a primary resistance and a leakage inductance from an input voltage vector of the induction motor, and a predetermined minute period immediately after starting to supply power to the induction motor At t1, the input current of the induction motor is set to be a DC current of zero or a value close to zero, and the center of an arc which is the locus of a magnetic flux vector output from the magnetic flux calculating means is obtained to determine the rotation angle of the induction motor. A first speed estimating means for estimating a frequency and a residual magnetic flux vector; and a case in which the speed cannot be estimated by the first speed estimating means. The center of an arc, which is the locus of the magnetic flux vector output from the magnetic flux calculating means, is determined by setting the input current of the motor to a predetermined DC current vector. The control apparatus for an induction motor for controlling the power converter for supplying power to the induction motor and a second speed estimation means for estimating a residual magnetic flux vector and the rotation angle frequency,
In the case where the speed cannot be estimated by the second speed estimating means, the DC current is caused to flow in the opposite direction to the current passed by the second speed estimating means immediately after the execution of the second speed estimating means. A control device for an induction motor, comprising: third speed estimating means for estimating a rotational angular frequency and a residual magnetic flux vector of the induction motor in the same manner as the second speed estimating means.
前記第1,第2または第3の速度推定手段において,前記磁束演算手段の出力の磁束ベクトルの軌跡である円弧の中心を求める際に,円弧の最初から最後までの時間を3等分して,それぞれの時間領域における円弧の平均値を計算して3点を求め,該3点を通る円の中心を求めて前記円弧の中心とすることを特徴とする請求項1記載の誘導電動機の制御装置。When the first, second or third speed estimating means finds the center of the arc which is the trajectory of the magnetic flux vector output from the magnetic flux calculating means, the time from the beginning to the end of the arc is divided into three equal parts. 2. The control of an induction motor according to claim 1, wherein an average value of the arcs in each time domain is calculated to determine three points, and a center of a circle passing through the three points is determined to be the center of the arc. apparatus. 前記第2または第3速度推定手段において,該第2または第3速度推定手段で流す直流電流ベクトルをixとし,該第2または第3速度推定手段で得られた速度に相当する角周波数をω0とし,前記誘導電動機の2次時定数をT2,相互インダクタンスをMとし,虚数単位をjで表して,前記磁束演算手段の出力の磁束ベクトルの軌跡である円弧の中心のベクトルをf0とし,前記第2または第3速度推定手段の最後の時点での前記磁束演算手段の出力の磁束ベクトルをf1として,残留磁束ベクトルφ0を,
φ0=M・ix/(1−j・ω0・T2)+f1−f0
により求める第2または第3速度推定手段を具備することを特徴とする請求項1又は2記載の誘導電動機の制御装置。
In the second or third speed estimating means, the dc current vector flowing by the second or third speed estimating means is ix, and the angular frequency corresponding to the speed obtained by the second or third speed estimating means is ω0 The secondary time constant of the induction motor is represented by T2, the mutual inductance is represented by M, the imaginary unit is represented by j, and the vector of the center of the arc which is the locus of the magnetic flux vector output from the magnetic flux computing means is represented by f0. The residual magnetic flux vector φ0 is defined as f1 as the magnetic flux vector output from the magnetic flux calculating means at the last time point of the second or third speed estimating means.
φ0 = M · ix / (1−j · ω0 · T2) + f1−f0
3. The control device for an induction motor according to claim 1, further comprising a second or third speed estimating unit obtained by the following.
前記第1速度推定手段の微少時間t1,および前記第2または第3速度推定手段の微少時間t2を,所定の最大時間と,前記磁束演算手段の出力の磁束ベクトルの軌跡である円弧の中心角が所定の角度になる時間との短い方の時間とすることを特徴とする請求項1、2又は3記載の誘導電動機の制御装置。The minute time t1 of the first speed estimating means and the minute time t2 of the second or third speed estimating means are defined as a predetermined maximum time and a central angle of an arc which is a locus of a magnetic flux vector output from the magnetic flux calculating means. 4. The control device for an induction motor according to claim 1, wherein the time is shorter than a time at which the angle becomes a predetermined angle.
JP09078499A 1999-03-31 1999-03-31 Induction motor control device Expired - Lifetime JP3566577B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP09078499A JP3566577B2 (en) 1999-03-31 1999-03-31 Induction motor control device

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP09078499A JP3566577B2 (en) 1999-03-31 1999-03-31 Induction motor control device

Publications (2)

Publication Number Publication Date
JP2000287491A JP2000287491A (en) 2000-10-13
JP3566577B2 true JP3566577B2 (en) 2004-09-15

Family

ID=14008237

Family Applications (1)

Application Number Title Priority Date Filing Date
JP09078499A Expired - Lifetime JP3566577B2 (en) 1999-03-31 1999-03-31 Induction motor control device

Country Status (1)

Country Link
JP (1) JP3566577B2 (en)

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP6021145B2 (en) * 2012-08-22 2016-11-09 東洋電機製造株式会社 Induction machine controller

Also Published As

Publication number Publication date
JP2000287491A (en) 2000-10-13

Similar Documents

Publication Publication Date Title
USRE40250E1 (en) Pulse width modulation circuit controlling output current of an inverter circuit for motor-driven blower or electric vacuum cleaner
JP2835039B2 (en) Elevator current / voltage controller
JP3719910B2 (en) Motor control device
JP7016762B2 (en) Semiconductor devices, motor drive systems, and motor control programs
JP2004166408A (en) Permanent magnet synchronous motor control method
WO2020175637A1 (en) Motor drive device, and air conditioner
CN105580267B (en) Power conversion device and power conversion method
JP5025142B2 (en) Motor control device
JP6759376B2 (en) Inverter controller
JP4050489B2 (en) Motor control method
JP3566577B2 (en) Induction motor control device
WO2018214979A1 (en) Control method for brushless dc motor, control device, and electric tool
JP2009165281A (en) Speed sensorless vector controller
JP2019208329A (en) Sensorless vector control device and sensorless vector control method
JP4032229B2 (en) AC motor control method and control apparatus
JP2002281795A (en) Controlling method for power refeeding to synchronous motor and controller for synchronous motor
JP3535735B2 (en) Induction motor control device
JP2003189673A (en) Motor control device
JP3508982B2 (en) AC motor control device
JP2004048840A (en) Controller of motor
JP2003284381A (en) Method of instantaneously interrupting and restarting induction motor and inverter control apparatus
JP2005110354A (en) Motor control method and motor control apparatus
JP3489259B2 (en) Permanent magnet type motor control method and control device
JP2004132282A (en) Lock detection method and device in compressor drive device
JP3979771B2 (en) AC motor control device

Legal Events

Date Code Title Description
A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20040315

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20040319

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20040607

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20040610

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20080618

Year of fee payment: 4

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20090618

Year of fee payment: 5

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20100618

Year of fee payment: 6

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20100618

Year of fee payment: 6

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20110618

Year of fee payment: 7

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20120618

Year of fee payment: 8

FPAY Renewal fee payment (event date is renewal date of database)

Free format text: PAYMENT UNTIL: 20130618

Year of fee payment: 9

EXPY Cancellation because of completion of term