CN1581670A - Method for positioning first-on rotor for alternating current permanent-magnet synchronous motor control system - Google Patents

Method for positioning first-on rotor for alternating current permanent-magnet synchronous motor control system Download PDF

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Publication number
CN1581670A
CN1581670A CNA2004100226108A CN200410022610A CN1581670A CN 1581670 A CN1581670 A CN 1581670A CN A2004100226108 A CNA2004100226108 A CN A2004100226108A CN 200410022610 A CN200410022610 A CN 200410022610A CN 1581670 A CN1581670 A CN 1581670A
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rotor
degree
interval
encoder
signal
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CN1279687C (en
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吕虹
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Guilin Stars Science And Technology Co ltd
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GUILIN STARS POWER ELECTRORNICS CO Ltd
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Abstract

General encoder and Hall component or increment type encoder capable of transmitting U, V, W signals are installed on rotor. U, V, W signals divide electrical angle of rotor position into six intervals in 60 degrees each. At strating up time of power on, magnetic vector intervals of rotor are determined through U, V, W signal states. The middle point of the interval is as position of magnetic vector of rotor. Controller outputs electrical current to three-phase winding of stator. Maximum phase error of current is only 30 degrees. When rotating rotor steps across interval, first change of U, V, W signal states occurs. Thus, accurate positioning for rotor is carried out, and normal operation begins. System checks position of rotor in every 60 degree in order to avoid positioning error in operation.

Description

The localization method of rotor when the AC permanent magnet synchronous motor control system powers on first
(1) technical field
The present invention relates to a kind of rotor localization method of AC permanent magnet synchronous motor control system, be specially the localization method of a kind of rotor of AC permanent magnet synchronous motor control system when powering on first.
(2) technical background
When AC permanent magnet synchronous motor is carried out SERVO CONTROL, the direction vector of controller control stator three-phase current resultant magnetic field.In order effectively to control stator flux vector, need accurately measure rotor-position.Usually economy and effective method is: incremental encoder is installed on rotor, is characterized the variation of rotor-position with the quantity of encoder output pulse.But in this method, the control computer of controller need obtain the initial position of rotor earlier, and the A that sends here according to encoder, B pulse could be determined the direction of rotor rotation and the angle of having rotated again.When system switched on first, the absolute position of rotor was uncertain.Use this quasi-controller when initially powering on, can only allow motor rotation earlier, when controller received the Z pulse that encoder sends here, controller could be confirmed the rotor-position initial point, that is to say could begin stator flux vector is begun to control.When motor is made, the Z pulse of encoder, i.e. the zero pulse of encoder all accurately is positioned the feature locations of rotor magnetic pole, as pole center line or magnetic field by the exchange point of N to S.When motor powered on first, the mechanical angle that rotor may need to turn over 360 degree just can search out zero point, receives the Z pulse of encoder, and beginning is control normally.This has reduced the operating efficiency of system, and some workplace does not allow rotor to turn over big angle motor like this and just enters operate as normal down as equipments such as military radar, cannons.
This problem is in the field of business drawing attention early.As Chinese patent 96106988 " detection method of original position of electric motor's rotator and device in the AC servo ", this invention can realize the measurement to original position of electric motor's rotator under the situation of control rotor rotary encoder one line, having overcome prior art needs open loop to rotate a circle to seek the shortcoming of initial zero-bit.But the examination method of gathering is adopted in this invention, change from small to large and measure motor rotation trend and come pointwise to seek the zero-bit of rotor by applying electric current, positioning time is long, the computing complexity, system complex, and in the motor location of can making a mistake under by extreme cases such as stalls.
(3) summary of the invention
Realize the rotor simple effective method of location fast when the objective of the invention is to design a kind of system and powering on first, normally start so that system can amount of exports when initially powering on decides torque.
The localization method of rotor when AC permanent magnet synchronous motor control system of the present invention powers on first, common incremental encoder is installed on rotor, the quantity of exporting A, B pulse with conventional coders characterizes the variation of rotor-position, the induction Hall element of rotor magnetic pole position is installed when motor is made in advance and is equipped with common incremental encoder simultaneously.The extraordinary incremental encoder of the supporting U of having, V, W signal perhaps is installed, and its installation method is identical with the installation of the induction Hall element of rotor magnetic pole position.U, the V that Hall element or this type of incremental encoder are sent, W status signal, have six level states, 101,100,110,010,011,001, per 360 of motor rotor position to be spent electrical degrees be divided into six equal intervals, each interval is 360 ÷ 6=60 ° electrical degrees.Initially powering on constantly, U, V, the W signal condition sent by incremental encoder, determine which interval is the rotor magnetic vector initially be positioned at, at this moment, get this interval mid point as the rotor field vector position, controller as the electric current of initial position of rotor to three-phase stator winding output respective vectors direction, guarantees that motor reaches nominal torque with this.
Because determined the interval at rotor vector place, and electrical degree that should the interval is 60 degree, so when getting the initial position of its mid point as the rotor vector, its error maximum has only 30 degree electrical degrees.Motor for sinusoidal wave torque angle displacement characteristic, stator feeds certain electric current, because the initial start moment error that the initial alignment error of 30 degree electrical degrees is brought is (1-Sin60 °) * 100%=13.4%, controller generally all has the overload capacity more than 20%, therefore under the situation of worst error 30 degree, still can export nominal torque when system initially powers on and normally start.For the motor of trapezoidal wave torque angle displacement characteristic, the initial start moment error of being brought by the initial alignment error is zero substantially.
After the motor operation that initially powers on, rotor has turned round certain angle (being 60 degree electrical degrees to the maximum) when having striden across the electrical degree interval, U, V, W state promptly take place to change for the first time, controller can accurately be located rotor according to the variation of U, V, W state immediately, and the A that sends according to encoder then, B pulse signal carry out operating rotor and accurately locate, thus the beginning commencement of commercial operation.
The advantage of rotor localization method was when AC permanent magnet synchronous motor control system of the present invention powered on first: 1, only need install additional and can send U, V, W signal Hall element or incremental encoder and can solve the AC permanent magnet synchronous motor control system and power on for the first time and can not accurately measure the problem of rotor-position, temporarily carry out coarse localization so that begin the driven operation immediately; 2, the position error maximum of utilizing this method just to locate is no more than ± 30 degree, guarantees normal startup operation in controller overload capacity scope; 3, after the normal operation of system, every running through 60 degree electrical degrees, system just can check the position of rotor, avoids in running, because the location mistake that encoder pulse error code or computer flight distance are brought.
(4) description of drawings
Fig. 1 is the schematic diagram of U, V, W characterization electrical angle of motor rotor position and the three-phase current oscillogram that export to three phase windings along controller according to U, V, W signal condition and variation back, rotor location.
(5) embodiment
Common incremental encoder is installed on rotor, is characterized the variation of rotor-position with the A of its output, the quantity of B pulse.Simultaneously the induction Hall element of rotor magnetic pole position is installed when motor is made in advance and is equipped with common incremental encoder, the extraordinary incremental encoder of the supporting U of having, V, W signal perhaps is installed.As shown in Figure 1, the U that Hall element or encoder are sent, V, W status signal have six level states, 101,100,110,010,011,001, what characterize the electrical angle of motor rotor position is six equally spaced intervals, and each interval is 360 ÷ 6=60 ° electrical degrees.Initially powering on constantly, U, V, the W signal condition sent by incremental encoder, promptly determine the residing interval of rotor magnetic vector initial position, get this interval mid point as the rotor field vector position, controller with this as initial position of rotor to the three-phase stator winding output current.
Rotor has been crossed over different electrical degrees when interval, when promptly turning over an electrical degree that is not more than 60 degree, and the once variation edge that must cross U, V, W state.And as long as rotor has been crossed the once variation edge of U, V, W state, U, V, W state take place to change for the first time, controller is accurately located rotor according to the variation of U, V, W state immediately, can accurately locate rotor, and the A that sends according to encoder then, B pulse signal carry out rotor and accurately locate, and motor promptly enters normal accurately positioning trip by the operation that initially powers on.
For the motor of 1 pair of utmost point, the electric angle that rotor turns over equates that with mechanical angle for the motor of N to the utmost point, the electric angle that rotor turns over equals N times of mechanical angle.Therefore adopt this method to carry out rotor and power on when locating, for the motor of N to the utmost point, the mechanical angle that rotor turns over before accurately locating is not more than N/one of 60 degree.
Above-mentioned U, V, W signal power on as the rotor location first except that being used for system, when system enters accurate location and normal operation, the rotor revolution is crossed 60 degree electrical degrees, must there be the state of a signal can take place once to change in U, V, the W signal, can does accurately location to the residing electrical degree of rotor according to the state of this saltus step and other two signals.Therefore can accurately locate again rotor-position by the edge of variation each time of U, V, W state, system can check the position of rotor, avoid in the running of this 60 degree electrical degree because the mistake that encoder pulse is lost or error code such as increase or computer flight distance are brought, as shown in Figure 1, guarantee the corresponding three-phase current waveform of controller respective rotor position to the output of three phase windings.

Claims (3)

  1. The localization method of rotor was installed conventional coders when 1 one kinds of AC permanent magnet synchronous motor controls powered on first on rotor, and the quantity of exporting A, B pulse with conventional coders characterizes the variation of rotor-position; It is characterized by:
    Simultaneously the induction Hall element of rotor magnetic pole position and the incremental encoder of outfit standard are installed in advance when motor is made, the incremental encoder of the supporting U of having, V, W signal perhaps is installed; The U that Hall element or encoder are sent, V, W status signal have six level states, and 101,100,110,010,011,001, what characterize the electrical angle of motor rotor position is six equally spaced intervals, each interval 60 degree electrical degree; Initially powering on constantly, U, V, the W signal condition sent by incremental encoder, determine the residing interval of rotor magnetic vector initial position, get this interval mid point as the rotor field vector position, controller with this as initial position of rotor to the three-phase stator winding output current;
    When the rotor running has striden across the electrical degree interval, U, V, W state take place to change for the first time, controller is accurately located rotor according to the variation of U, V, W state immediately, and the A that sends according to encoder then, B pulse signal carry out rotor and accurately locate the beginning commencement of commercial operation.
  2. The localization method of rotor when 2 AC permanent magnet synchronous motor controls according to claim 1 power on first is characterized by:
    When system enters accurate location and normal operation, the rotor revolution is crossed 60 degree electrical degrees, have the state of a signal can take place once to change in U, V, the W signal, according to the state of this saltus step and other two signals the residing electrical degree of rotor is done accurately location, system checks the position of rotor.
  3. The localization method of rotor when 3 AC permanent magnet synchronous motor controls according to claim 1 power on first is characterized by:
    For the motor of N to the utmost point, the mechanical angle that rotor turns over before accurately locating is not more than N/one of 60 degree.
CNB2004100226108A 2004-05-18 2004-05-18 Method for positioning first-on rotor for alternating current permanent-magnet synchronous motor control system Expired - Lifetime CN1279687C (en)

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Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101273519B (en) * 2005-08-30 2011-05-25 霍尼韦尔国际公司 Method of operating a brushless DC motor
CN101621274B (en) * 2009-06-29 2011-09-28 中国兵器工业第五八研究所 Method for automatically recognizing AC servo motor in AC servo system
CN101651442B (en) * 2008-08-15 2011-09-28 深圳市汇川技术股份有限公司 Method and system for correcting electrical angle of motor rotor
CN102510254A (en) * 2011-11-07 2012-06-20 郑州飞机装备有限责任公司 Initial alignment method of permanent magnetic synchronous motor rotor of pure electric vehicle
CN103697927A (en) * 2012-09-27 2014-04-02 现代摩比斯株式会社 Position sensor abnormality detection method of a smart booster system
CN101050729B (en) * 2007-04-23 2014-12-03 桂林星辰电力电子有限公司 Energy distribution type servo system matched with fuel engine and its regulating method
CN105720870A (en) * 2016-04-11 2016-06-29 苏州正弦波机电科技有限公司 Sensorless starting method for automobile air conditioner
CN106533308A (en) * 2016-12-31 2017-03-22 深圳市优必选科技有限公司 Angle detection method and device for permanent magnet synchronous motor
CN106817061A (en) * 2015-11-27 2017-06-09 沈阳高精数控智能技术股份有限公司 A kind of method for detecting initial position of rotor
CN106849810A (en) * 2017-03-31 2017-06-13 深圳市伟创电气有限公司 The initial position detection method and device of AC permanent magnet synchronous motor rotor
CN108120454A (en) * 2016-11-28 2018-06-05 沈阳新松机器人自动化股份有限公司 A kind of angle detecting method of incremental encoder
CN108120455A (en) * 2016-11-28 2018-06-05 姜国超 Encoder based on the digital analogue signal combination that Hall sensor generates
CN109600092A (en) * 2018-12-17 2019-04-09 北京无线电测量研究所 A kind of monitoring of permanent-magnet synchronous motor rotor position and modification method, system and motor
CN109983690A (en) * 2016-11-22 2019-07-05 舍弗勒技术股份两合公司 Method and circuit arrangement for determining the position of a rotor of an electric motor
CN110463020A (en) * 2018-07-02 2019-11-15 深圳市大疆创新科技有限公司 The acquisition methods and system of the initial mechanical angle of motor

Cited By (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101273519B (en) * 2005-08-30 2011-05-25 霍尼韦尔国际公司 Method of operating a brushless DC motor
CN101050729B (en) * 2007-04-23 2014-12-03 桂林星辰电力电子有限公司 Energy distribution type servo system matched with fuel engine and its regulating method
CN101651442B (en) * 2008-08-15 2011-09-28 深圳市汇川技术股份有限公司 Method and system for correcting electrical angle of motor rotor
CN101621274B (en) * 2009-06-29 2011-09-28 中国兵器工业第五八研究所 Method for automatically recognizing AC servo motor in AC servo system
CN102510254A (en) * 2011-11-07 2012-06-20 郑州飞机装备有限责任公司 Initial alignment method of permanent magnetic synchronous motor rotor of pure electric vehicle
CN103697927B (en) * 2012-09-27 2017-10-31 现代摩比斯株式会社 The position detector method for detecting abnormality of Intelligent booster system
CN103697927A (en) * 2012-09-27 2014-04-02 现代摩比斯株式会社 Position sensor abnormality detection method of a smart booster system
CN106817061A (en) * 2015-11-27 2017-06-09 沈阳高精数控智能技术股份有限公司 A kind of method for detecting initial position of rotor
CN106817061B (en) * 2015-11-27 2019-05-14 沈阳高精数控智能技术股份有限公司 A method of detection initial position of rotor
CN105720870A (en) * 2016-04-11 2016-06-29 苏州正弦波机电科技有限公司 Sensorless starting method for automobile air conditioner
CN109983690A (en) * 2016-11-22 2019-07-05 舍弗勒技术股份两合公司 Method and circuit arrangement for determining the position of a rotor of an electric motor
CN108120455A (en) * 2016-11-28 2018-06-05 姜国超 Encoder based on the digital analogue signal combination that Hall sensor generates
CN108120454A (en) * 2016-11-28 2018-06-05 沈阳新松机器人自动化股份有限公司 A kind of angle detecting method of incremental encoder
CN108120454B (en) * 2016-11-28 2020-09-29 沈阳新松机器人自动化股份有限公司 Angle detection method of incremental encoder
CN106533308A (en) * 2016-12-31 2017-03-22 深圳市优必选科技有限公司 Angle detection method and device for permanent magnet synchronous motor
CN106533308B (en) * 2016-12-31 2019-10-29 深圳市优必选科技有限公司 Angle detection method and device for permanent magnet synchronous motor
CN106849810A (en) * 2017-03-31 2017-06-13 深圳市伟创电气有限公司 The initial position detection method and device of AC permanent magnet synchronous motor rotor
CN110463020A (en) * 2018-07-02 2019-11-15 深圳市大疆创新科技有限公司 The acquisition methods and system of the initial mechanical angle of motor
CN109600092A (en) * 2018-12-17 2019-04-09 北京无线电测量研究所 A kind of monitoring of permanent-magnet synchronous motor rotor position and modification method, system and motor
CN109600092B (en) * 2018-12-17 2020-11-27 北京无线电测量研究所 Permanent magnet synchronous motor rotor position monitoring and correcting method and system and motor

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