CN104767446B - A kind of hybrid exciting synchronous motor air-gap flux and electric current phasor angle control method - Google Patents

A kind of hybrid exciting synchronous motor air-gap flux and electric current phasor angle control method Download PDF

Info

Publication number
CN104767446B
CN104767446B CN201510170421.3A CN201510170421A CN104767446B CN 104767446 B CN104767446 B CN 104767446B CN 201510170421 A CN201510170421 A CN 201510170421A CN 104767446 B CN104767446 B CN 104767446B
Authority
CN
China
Prior art keywords
shaft
current
exciting
psi
synchronous motor
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 - Fee Related
Application number
CN201510170421.3A
Other languages
Chinese (zh)
Other versions
CN104767446A (en
Inventor
林明耀
赵纪龙
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.)
Southeast University
Original Assignee
Southeast University
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 Southeast University filed Critical Southeast University
Priority to CN201510170421.3A priority Critical patent/CN104767446B/en
Publication of CN104767446A publication Critical patent/CN104767446A/en
Application granted granted Critical
Publication of CN104767446B publication Critical patent/CN104767446B/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Control Of Ac Motors In General (AREA)

Abstract

The invention discloses a kind of hybrid exciting synchronous motor air-gap flux and electric current phasor angle control method, by controlling d shaft currents id, q shaft currents iqWith exciting current if, keep air-gap flux to be equal to 90 ° with electric current phasor angle θ.Motor operation controls i according to load control in low regimed、iqAnd ifθ is made to be equal to 90 °.When load torque is less than nominal torque, exciting current is 0, by controlling idAnd iqθ is made to be equal to 90 °;When load torque is more than nominal torque, by coordinating id、iqAnd ifθ is made to be equal to 90 °.Motor operation when high velocity, using idWith ifCommon weak magnetic, by id、iqAnd ifCoordinate control θ and be equal to 90 °.Hybrid exciting synchronous motor air-gap flux makes the capacity of inverter be fully used with electric current phasor angle control method, and relatively low to stator voltage and voltammetric capacity requirement, is particularly well-suited to high-power and Large Copacity governing system.

Description

A kind of hybrid exciting synchronous motor air-gap flux and electric current phasor angle control method
Technical field
The invention belongs to electric drive technology field, is related to a kind of air-gap flux and electric current phasor angle control policy, especially It is to be related to a kind of hybrid exciting synchronous motor control method.
Background technology
Hybrid exciting synchronous motor is that the one kind grown up on the basis of permanent-magnet synchronous with electric excitation synchronous motor is wide Buncher, its main purpose are to solve the problems, such as that permagnetic synchronous motor air-gap field is difficult to adjust.Composite excitation synchronization Motor has two kinds of excitation sources, and one kind is permanent magnet, and another kind is electrical excitation, magnetic potential based on the magnetic potential that permanent magnet is produced, excitation Magnetic potential supplemented by the magnetic potential that winding is produced.This motor combines the advantage of permanent-magnet synchronous and electric excitation synchronous motor, two kinds of excitations Source interacts in motor gas-gap and produces main flux, when electrical excitation coil is passed through the exciting current of forward direction, produces positive electricity Magnetic torque and increase motor torque;Conversely, when electrical excitation coil is passed through reverse exciting current, then producing opposing magnetic field and weakening Air-gap field reaches the purpose of weak magnetic speed-up, so as to widen the speed adjustable range of motor.
At present, it is less for hybrid exciting synchronous motor control method and Research on Driving System both at home and abroad, related data It is not a lot.Based on vector controlled, four classes can be classified as substantially, one is id=0 control, two is weak magnetic control, and three is that efficiency is excellent Change control, four is unity power factor control.The advantage of first three class control method is simple and convenient, output-constant operation wide ranges, Row area efficiency for the national games is high;Have the disadvantage the problems such as power factor is reduced, and terminal voltage is raised.Although unity power factor control is improved The power factor of control system, but voltammetric capacity has high demands, and equally stator voltage is required also higher.And both at home and abroad for mixed Close excitation magnetic synchronization motor air-gap flux space state is substantially at the control research of electric current phasor angle.
The content of the invention
Technical problem:The present invention proposes one kind, and no matter hybrid exciting synchronous motor operates in low regime or high velocity, Air-gap flux and electric current phasor angle are all kept equal to 90 °, reduce control system to the demand of stator voltage and voltammetric capacity, carry The hybrid exciting synchronous motor air-gap flux and electric current phasor angle control method of high grid power transmission efficiency.
Technical scheme:Hybrid exciting synchronous motor air-gap flux and the electric current phasor angle control method of the present invention, including with Lower step:
(1) phase current i is gathered from motor main circuita、ibWith exciting current if, initial position detection is carried out to motor, from electricity Signal is gathered on machine encoder, controller is sent into and is processed, draw rotating speed n and rotor position angle θ;
(2) by the phase current i of collectiona、ibJing is followed, is filtered, biasing and A/D conversions, is then carried out park transforms, is obtained Stator d shaft currents i under two-phase rotating coordinate systemdWith q shaft currents iq
(3) use given rotating speed n*Encoder actual measurement rotating speed n is deducted, by the rotating speed deviation △ n input speed actuators for obtaining, Torque reference value is obtained Jing after proportional integral computingBy torque reference valueActual measurement rotating speed n and given rotating speed n*Input current According to rotating speed, allotter, judges that motor operation is interval:When actual speed is less than rated speed, then hybrid exciting synchronous motor is transported In low regime, into step (4), otherwise, hybrid exciting synchronous motor runs on high velocity to row, into step (5);
(4) judge whether load torque meets TL≤TN, wherein TLFor load torque, TNFor nominal torque;
Work as TL≤TNWhen, magnetic control, i need not be increasedfref=0, keep the angle theta between air gap synthesis magnetic linkage and electric current phasor Equal to 90 °, solved according to following equations group and calculate d shaft current reference values idref, q shaft current reference values iqrefJoin with exciting current Examine value ifref, the current sharing scheme output current that distributing switch is obtained according to solution, subsequently into step (6):
Work as TL>TNWhen, increasing magnetic control is carried out, is solved according to following equations group and is calculated d shaft current reference values idref, q shaft currents Reference value iqrefWith exciting current reference value ifref, the current sharing scheme output current that distributing switch is obtained according to solution, so Step (6) is entered afterwards:
Wherein, ψexcm+Mfifref, idrefFor d shaft current reference values, iqrefFor q shaft current reference values, ifrefFor excitation Current reference value;ψmFor permanent magnet flux linkage, p is motor number of pole-pairs;IfNFor exciting current rated value, Ld、LqRespectively stator winding D axles and q axle inductances, MfFor the mutual inductance between armature winding and Exciting Windings for Transverse Differential Protection, TerefFor electromagnetic torque reference value;
(5) using d shaft currents idWith exciting current ifWeak magnetic, keeps between air gap synthesis magnetic linkage and electric current phasor simultaneously Angle theta be equal to 90 °, distributing switch according to following current sharing scheme output current, into step (6):
Wherein, ωeFor angular rate, UdcFor busbar voltage;
(6) with d shaft current reference values i produced by distributing switchdrefDeduct d shaft currents i in step (2)dObtain d Shaft current deviation △ id, with q shaft current reference values iqrefDeduct q shaft currents i in step (2)qObtain q shaft current deviation △ iq, By the d shaft current deviations △ idInput d shaft currents actuator carries out proportional integral computing, obtains d shaft voltage ud, by the q axles Current deviation △ iqInput q shaft currents actuator carries out proportional integral computing, obtains q shaft voltage uq, then to the d shaft voltages udWith q shaft voltage uqAfter carrying out jointly rotating orthogonal-static two phase inversion, α shaft voltage u under static two phase coordinate system are obtainedαAnd β Shaft voltage uβ, by the α shaft voltages uαWith β shaft voltage uβInput pulse width modulation module, 6 tunnel pulse width of computing output are adjusted Signal processed, drives main power inverter;
Simultaneously by the exciting current i of collection in step (1)f, Jing follow, filter, bias with A/D conversion after and exciting current Reference value ifrefDC excitation pulse width modulation module is sent into together, and computing exports 4 road pulse width modulating signals to drive excitation Power inverter.In a kind of preferred version of the inventive method, step 6) in Pulse width modulation module be space vector arteries and veins Rush width modulation module.
Beneficial effect:The i of existing hybrid exciting synchronous motord=0 and efficiency-optimized control method there are shortcomings, its One of be exactly that the power factor of motor reduces therewith with the increase of load;Although unity power factor control improves control The power factor of system processed, but while stator voltage and voltammetric capacity are required higher.The present invention passes through step (4) and step (5) air-gap flux and electric current phasor angle control method, make no matter hybrid exciting synchronous motor operates in low regime or high speed Area, all keeps air-gap flux to be equal to 90 ° with electric current phasor angle.The control method is at aspects such as output torque, efficiency, power factors The characteristics of and unity power factor control relatively, but the requirement much lower to electric moter voltage and voltammetric capacity, thus this The relatively existing control method of invention has advantages below:
The power factor of the method control system is about 1, makes inverter be fully used, and improves the transmission of electricity effect of electrical network Rate;
It is 1 control relative to power factor, this method reduces demand of the control system to stator voltage;
It is 1 control relative to power factor, this method reduces demand of the control system to voltammetric capacity;
So hybrid exciting synchronous motor air-gap flux and electric current phasor angle control Large Copacity, high-power speed-adjusting system, There is certain application prospect in high-speed electric expreess locomotive field.
Description of the drawings
Fig. 1 is the logical procedure diagram of the inventive method;
Fig. 2 is the system block diagram of the inventive method;
Fig. 3 is the structured flowchart for realizing the inventive method;
Fig. 4 is hybrid exciting synchronous motor vector diagram.
Specific embodiment
With reference to embodiment and Figure of description, the present invention is further illustrated.
Fig. 3 is the system frame for realizing hybrid exciting synchronous motor air-gap flux of the present invention and electric current phasor angle control method Figure, the control system by alternating current power supply, commutator, electric capacity of voltage regulation, dsp controller, main power inverter, auxiliary power inverter, Sensor, hybrid exciting synchronous motor, photoelectric encoder etc. are constituted.
Alternating current power supply is powered to whole system, and after rectifier rectification, main and auxiliary power conversion is given in filtering, voltage stabilizing Device, Hall voltage sensor collection busbar voltage, sends into controller after conditioning.The output termination mixing of main and auxiliary power inverter Excitation magnetic synchronization motor, Hall current transformer collection phase current and exciting current, send into controller after conditioning, code device signal is adopted Collection rotating speed and rotor-position signal, send into controller and calculate rotor position angle and rotating speed after process.Controller exports 10 road PWM letters Main, exciting power changer is driven number respectively.
The hybrid exciting synchronous motor air-gap flux of the present invention controls control method with electric current phasor angle, shown in Fig. 3, specifically Comprise the following steps:
(1) three Hall current sensor gathers phase current i from motor main circuit respectivelya、ibWith exciting current if, will adopt The signal for collecting sends into controller Jing after the signal conditions such as voltage follow, filtering, biasing and overvoltage protection, and motor is carried out accurately Initial position detection, gathers signal from motor encoder, processes feeding controller and calculates rotating speed n and rotor position angle θ;
(2) will be fed into the phase current i of controllera、ibA/D conversions are carried out, through three phase coordinate systems to two-phase rotating coordinate system Park transforms obtain d shaft currents i under two-phase rotating coordinate systemdWith q shaft currents iq
(3) use given rotating speed n*Deduct encoder actual measurement rotating speed n, after obtain rotating speed deviation △ n, rotating speed deviation △ n is entered Torque reference value is obtained after speed regulatorBy torque reference valueActual measurement rotating speed n and given rotating speed n*Send into electric current distribution Whether device, judge actual speed less than rated speed, and in this way, motor operation in low regime, into step (4), otherwise, transport by motor Go in high velocity, into step (5);
(4) judge whether load torque meets TL≤TN, TLFor load torque, TNFor nominal torque;
Lower surface analysis low regime hybrid exciting synchronous motor air-gap flux and electric current phasor angle control principle, according to vector control Principle processed, in d-q coordinate systems, draws the mathematical model of hybrid exciting synchronous motor.
Flux linkage equations:
Voltage equation:
Electromagnetic torque equation:
Wherein, id、iqRespectively d axles and q shaft currents, IsFor rated current, ifFor exciting current;Ld、LqRespectively d axles with Q axle inductances, MfFor the mutual inductance between armature and Exciting Windings for Transverse Differential Protection;ωeFor angular rate;ψmFor permanent magnet flux linkage, p is that motor is extremely right Number, ud、uqThe respectively voltage of d axles and q axles, ufFor Exciting Windings for Transverse Differential Protection voltage;RsFor armature winding resistance, RfFor Exciting Windings for Transverse Differential Protection electricity Resistance;ψd、ψq、ψfDifference d axles, q axles and Exciting Windings for Transverse Differential Protection magnetic linkage;TeFor electromagnetic torque.
Hybrid exciting synchronous motor phasor diagram is as shown in figure 4, it can be seen that can obtain following equation
According to formula (4), electromagnetic torque TeCan be expressed as
Wherein, θ is the angle that air gap synthesizes between magnetic linkage and electric current phasor, and δ is power angle, and β is angle of torsion, ψsFor air gap Synthesis magnetic linkage, isFor stator current vector.
From formula (5) as can be seen that the angle theta between control air gap synthesis magnetic linkage and electric current phasor can just control electromagnetism turn Square.
The invention control air gap synthesis magnetic linkage and electric current phasor angle θ=90 °, can obtain
So as to obtain
Sin β=cos δ (7)
Work as TL≤TNWhen, magnetic control need not be increased, so exciting current if=0, θ=90 ° are kept, is obtained
D shaft current reference values i are calculated according to above formuladref, q shaft current reference values iqrefWith exciting current reference value ifrefFor
Electric current distribution is carried out according to above formula, step (6) is directly entered.
Work as TL>TNWhen, increasing magnetic control is carried out, θ=90 ° is kept, can be obtained
Wherein, ψexcm+Mfifref
D shaft current reference values i are calculated according to above formula thendref, q shaft current reference values iqrefWith exciting current reference value ifref For
Electric current distribution is carried out according to above formula, step (6) is directly entered.
(5) using d shaft currents idWith exciting current ifWeak magnetic, keeps θ=90 ° simultaneously, and it is anti-electric that weak magnetic calculating formula ignores d axles Gesture, then have
D shaft current reference values i are calculated according to above formuladref, q shaft current reference values iqrefWith exciting current reference value ifrefFor
Electric current distribution is carried out according to above formula, step (6) is directly entered.
(6) with d shaft current reference values i produced by distributing switchdrefDeduct d shaft currents i in step (2)dObtain d Shaft current deviation △ id, with q shaft current reference values iqrefDeduct q shaft currents i in step (2)qObtain q shaft current deviation △ iq, By d shaft current deviation △ idInput d shaft currents actuator carries out proportional integral computing, obtains d shaft voltage ud, by q shaft current deviations △iqInput q shaft currents actuator carries out proportional integral computing, obtains q shaft voltage uq, then to the d shaft voltages udWith q axles electricity Pressure uqAfter carrying out jointly rotating orthogonal-static two phase inversion, α shaft voltage u under static two phase coordinate system are obtainedαWith β shaft voltage uβ, By the α shaft voltages uαWith β shaft voltage uβInput pulse width modulation module, computing export 6 road pulse width modulating signals, drive Move main power inverter;Simultaneously by the exciting current i of collection in step (1)f, Jing follow, filter, bias with A/D conversion after and Exciting current reference value ifrefDC excitation pulse width modulation module is sent into together, and computing exports 4 road pulse width modulating signals and comes Drive exciting power changer.
Above-described embodiment is only the preferred embodiment of the present invention, it should be pointed out that:For the ordinary skill of the art For personnel, under the premise without departing from the principles of the invention, some improvement and equivalent can also be made, these are to the present invention Claim is improved and the technical scheme after equivalent, each falls within protection scope of the present invention.

Claims (2)

1. a kind of hybrid exciting synchronous motor air-gap flux and electric current phasor angle control method, it is characterised in that the method includes Following steps:
(1) phase current i is gathered from motor main circuita、ibWith exciting current if, initial position detection is carried out to motor, is compiled from motor Signal is gathered on code device, controller is sent into and is processed, draw rotating speed n and rotor position angle θ;
(2) by the phase current i of collectiona、ibJing is followed, is filtered, biasing and A/D conversions, is then carried out park transforms, is obtained biphase Stator d shaft currents i under rotating coordinate systemdWith q shaft currents iq
(3) use given rotating speed n*Encoder actual measurement rotating speed n is deducted, by the rotating speed deviation △ n input speed actuators for obtaining, Jing ratios Torque reference value is obtained after example integral operationBy torque reference valueActual measurement rotating speed n and given rotating speed n*Input current distributes According to rotating speed, device, judges that motor operation is interval:When actual speed is less than rated speed, then hybrid exciting synchronous motor runs on Low regime, into step (4), otherwise, hybrid exciting synchronous motor runs on high velocity, into step (5);
(4) judge whether load torque meets TL≤TN, wherein TLFor load torque, TNFor nominal torque;
Work as TL≤TNWhen, magnetic control, i need not be increasedfref=0, keep the angle theta between air gap synthesis magnetic linkage and electric current phasor to be equal to 90 °, solved according to following equations group and calculate d shaft current reference values idref, q shaft current reference values iqrefWith exciting current reference value ifref, the current sharing scheme output current that distributing switch is obtained according to solution, subsequently into step (6):
i d r e f = - ψ m - ψ m 2 + 4 L d L q i q r e f 2 2 L d i q r e f = 2 T e r e f 3 p [ ψ m + ( L d - L q ) ( - ψ m - ψ m 2 + 4 L d L q i q r e f 2 2 L d ) ] i f r e f = 0
Work as TL>TNWhen, increasing magnetic control is carried out, is solved according to following equations group and is calculated d shaft current reference values idref, q shaft currents reference Value iqrefWith exciting current reference value ifref, the current sharing scheme output current that distributing switch is obtained according to solution, Ran Houjin Enter step (6):
i d r e f = - ψ e x c - ψ e x c 2 + 4 L d L q i q r e f 2 2 L d i q r e f = 2 T e r e f 3 p [ ψ e x c + ( L d - L q ) ( - ψ e x c - ψ e x c 2 + 4 L d L q i q r e f 2 2 L d ) ] i f r e f = I f N
Wherein, ψexcm+Mfifref, idrefFor d shaft current reference values, iqrefFor q shaft current reference values, ifrefFor exciting current Reference value;ψmFor permanent magnet flux linkage, p is motor number of pole-pairs;IfNFor exciting current rated value, Ld、LqRespectively stator winding d axles With q axle inductances, MfFor the mutual inductance between armature winding and Exciting Windings for Transverse Differential Protection, TerefFor electromagnetic torque reference value;
(5) using d shaft currents idWith exciting current ifWeak magnetic, keeps the angle theta between air gap synthesis magnetic linkage and electric current phasor simultaneously Equal to 90 °, distributing switch according to following current sharing scheme output current, into step (6):
i d r e f = U d c 3 ω e - ( ψ m + M f i f r e f ) L d i q r e f = i d r e f [ ψ m + L d i d r e f + M f i f r e f ] L q i f r e f = 2 T e r e f 3 pi q r e f - [ ψ m + i d r e f ( L d - L q ) ] M f
Wherein, ωeFor angular rate, UdcFor busbar voltage;
(6) with d shaft current reference values i produced by distributing switchdrefDeduct d shaft currents i in step (2)dObtain d axles electricity Stream deviation △ id, with q shaft current reference values iqrefDeduct q shaft currents i in step (2)qObtain q shaft current deviation △ iq, by institute State d shaft current deviation △ idInput d shaft currents actuator carries out proportional integral computing, obtains d shaft voltage ud, by the q shaft currents Deviation △ iqInput q shaft currents actuator carries out proportional integral computing, obtains q shaft voltage uq, then to the d shaft voltages udAnd q Shaft voltage uqAfter carrying out jointly rotating orthogonal-static two phase inversion, α shaft voltage u under static two phase coordinate system are obtainedαWith β shaft voltages uβ, by the α shaft voltages uαWith β shaft voltage uβInput pulse width modulation module, computing export 6 road pulse width modulating signals, Drive main power inverter;
Simultaneously by the exciting current i of collection in step (1)f, refer to exciting current Jing following, filtering, bias with after A/D conversions Value ifrefDC excitation pulse width modulation module is sent into together, and computing exports 4 road pulse width modulating signals to drive exciting power Changer.
2. hybrid exciting synchronous motor air-gap flux according to claim 1 and electric current phasor angle control method, its feature Be, the step 6) in Pulse width modulation module be space vector pulse width modulation module.
CN201510170421.3A 2015-04-10 2015-04-10 A kind of hybrid exciting synchronous motor air-gap flux and electric current phasor angle control method Expired - Fee Related CN104767446B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201510170421.3A CN104767446B (en) 2015-04-10 2015-04-10 A kind of hybrid exciting synchronous motor air-gap flux and electric current phasor angle control method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201510170421.3A CN104767446B (en) 2015-04-10 2015-04-10 A kind of hybrid exciting synchronous motor air-gap flux and electric current phasor angle control method

Publications (2)

Publication Number Publication Date
CN104767446A CN104767446A (en) 2015-07-08
CN104767446B true CN104767446B (en) 2017-04-05

Family

ID=53649110

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201510170421.3A Expired - Fee Related CN104767446B (en) 2015-04-10 2015-04-10 A kind of hybrid exciting synchronous motor air-gap flux and electric current phasor angle control method

Country Status (1)

Country Link
CN (1) CN104767446B (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN105024606A (en) * 2015-07-13 2015-11-04 东菱技术有限公司 Intelligent motor driving method for high-voltage circuit breaker
CN107154765B (en) * 2017-05-11 2019-03-29 东南大学 A kind of Magneticflux-switching type memory electrical machine High Power Factor control method
CN112769366B (en) * 2020-12-31 2024-01-09 江苏国传电气有限公司 Method, device and system for controlling excitation current transformer of electric excitation synchronous motor
CN114719403B (en) * 2022-04-26 2023-03-28 珠海格力电器股份有限公司 Compressor frequency reduction control method, device and unit

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101159422A (en) * 2007-10-16 2008-04-09 李平 Permanent-magnet DC motor drive control system with approximate constant power pulling motor characteristics
CN103607156A (en) * 2013-11-25 2014-02-26 东南大学 Method for controlling power factor of mixed excitation synchronous motor
CN103647489A (en) * 2013-12-12 2014-03-19 东南大学 Hybrid excitation synchronous motor efficiency optimized control method

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP5862125B2 (en) * 2011-09-05 2016-02-16 富士電機株式会社 Control device for power converter

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101159422A (en) * 2007-10-16 2008-04-09 李平 Permanent-magnet DC motor drive control system with approximate constant power pulling motor characteristics
CN103607156A (en) * 2013-11-25 2014-02-26 东南大学 Method for controlling power factor of mixed excitation synchronous motor
CN103647489A (en) * 2013-12-12 2014-03-19 东南大学 Hybrid excitation synchronous motor efficiency optimized control method

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
混合励磁同步电机及其控制技术综述和新进展;赵纪龙等;《中国电机工程学报》;20141125;第34卷(第33期);第5867-5887页 *

Also Published As

Publication number Publication date
CN104767446A (en) 2015-07-08

Similar Documents

Publication Publication Date Title
CN103647489B (en) A kind of hybrid exciting synchronous motor efficiency-optimized control method
CN104682806B (en) Constant flux linkage control method for hybrid excitation synchronous motor
CN105515479B (en) A kind of durface mounted permanent magnet synchronous generator field weakening control method
CN106788081B (en) A kind of minimum Direct Torque Control of hybrid exciting synchronous motor loss
CN104378035A (en) Mixed excitation synchronous motor field weakening control method for judging field weakening moment through voltage differences
CN102223133B (en) Maximum torque control method for salient-pole permanent-magnet synchronous motor
CN103997267B (en) A kind of series compensation Direct Torque Control of driving winding permanent magnet synchronous motor
CN104767446B (en) A kind of hybrid exciting synchronous motor air-gap flux and electric current phasor angle control method
CN103401506B (en) A kind of direct torque control method for non-salient pole type hybrid excitation motor for electric vehicle
CN103441726A (en) Double three-phase permanent magnet motor vector control method based on proportional resonance regulator
CN102645632A (en) Efficiency test system and control method for no-angle sensor of permanent magnet synchronous motor
CN105099316B (en) A kind of electric current control method for coordinating of electric excitation synchronous motor
CN103944478B (en) A kind of AC excitation synchronous motor control device and method
CN102412778A (en) Full speed domain torque maximizing vector control current distribution method for induction motor
CN104767455A (en) Hybrid excitation synchronous motor sensorless direct torque control method
CN103595324B (en) A kind of mixed excitation electric machine field weakening control method
CN108390602A (en) A kind of direct prediction power control method of hybrid exciting synchronous motor
CN104617849B (en) A kind of hybrid exciting synchronous motor peak power output control method
CN201197132Y (en) Vector control AC variable-frequency control system of electric car
CN107623469A (en) The weak magnetic control device and method of a kind of direct current biasing sinusoidal current motor
CN101264737B (en) Electric automobile vector control AC variable-frequency speed regulation system
CN104617827A (en) Method for controlling fault tolerance of axial magnetic field flux-switching permanent motor of electric vehicle
CN103607156B (en) A kind of hybrid exciting synchronous motor power factor control method
CN103840732B (en) Drive motors field weakening control method
CN107947669B (en) Nonlinear back-thrust tracking control method for hybrid excitation synchronous motor

Legal Events

Date Code Title Description
C06 Publication
PB01 Publication
EXSB Decision made by sipo to initiate substantive examination
SE01 Entry into force of request for substantive examination
GR01 Patent grant
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20170405