Vector Control of a 3-Phase AC Induction Motor Using the ZNEO Multimotor Z16FMC MCU Series AN037803-0117
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Naval Postgraduate School
NPS-97-06-003 NAVAL POSTGRADUATE SCHOOL MONTEREY, CALIFORNIA SHIP ANTI BALLISTIC MISSILE RESPONSE (SABR) by LT Allen P. Johnson LT David C. Leiker LT Bryan Breeden ENS Parker Carlisle LT Willard Earl Duff ENS Michael Diersing LT Paul F. Fischer ENS Ryan Devlin LT Nathan Hornback ENS Christopher Glenn TDSI Students LT Chris Hoffmeister, USN LT John Kelly, USN LTC Tay Boon Chong, SAF LTC Yap Kwee Chye, SAF MAJ Phang Nyit Sing, SAF CPT Low Wee Meng, SAF CPT Ang Keng-ern, SAF CPT Ohad Berman, IDF Mr. Fann Chee Meng, DSTA, Singapore Mr. Chin Chee Kian, DSTA, Singapore Mr. Yeo Jiunn Wah, DSTA, Singapore June 2006 Approved for public release; distribution is unlimited. Prepared for: Deputy Chief of Naval Operations for Warfare Requirements and Programs (OPNAV N7), 2000 Navy Pentagon, Rm. 4E392, Washington, D.C. 20350-2000 THIS PAGE INTENTIONALLY LEFT BLANK REPORT DOCUMENTATION PAGE Form Approved OMB No. 0704-0188 Public reporting burden for this collection of information is estimated to average 1 hour per response, including the time for reviewing instruction, searching existing data sources, gathering and maintaining the data needed, and completing and reviewing the collection of information. Send comments regarding this burden estimate or any other aspect of this collection of information, including suggestions for reducing this burden, to Washington Headquarters Services, Directorate for Information Operations and Reports, 1215 Jefferson Davis Highway, Suite 1204, Arlington, VA 22202-4302, and to the Office of Management and Budget, Paperwork Reduction Project (0704-0188) Washington, DC 20503. 1. AGENCY USE ONLY (Leave blank) 2. REPORT DATE 3. -
Direct Torque Control of Induction Motors
DIRECT TORQUE CONTROL FOR INDUCTION MOTOR DRIVES MAIN FEATURES OF DTC · Decoupled control of torque and flux · Absence of mechanical transducers · Current regulator, PWM pulse generation, PI control of flux and torque and co-ordinate transformation are not required · Very simple control scheme and low computational time · Reduced parameter sensitivity BLOCK DIAGRAM OF DTC SCHEME + _ s* s j s + Djs _ Voltage Vector s * T + j s DT Selection _ T S S S s Stator a b c Torque j s s E Flux vs 2 Estimator Estimator 3 s is 2 i b i a 3 Induction Motor In principle the DTC method selects one of the six nonzero and two zero voltage vectors of the inverter on the basis of the instantaneous errors in torque and stator flux magnitude. MAIN TOPICS Þ Space vector representation Þ Fundamental concept of DTC Þ Rotor flux reference Þ Voltage vector selection criteria Þ Amplitude of flux and torque hysteresis band Þ Direct self control (DSC) Þ SVM applied to DTC Þ Flux estimation at low speed Þ Sensitivity to parameter variations and current sensor offsets Þ Conclusions INVERTER OUTPUT VOLTAGE VECTORS I Sw1 Sw3 Sw5 E a b c Sw2 Sw4 Sw6 Voltage-source inverter (VSI) For each possible switching configuration, the output voltages can be represented in terms of space vectors, according to the following equation æ 2p 4p ö s 2 j j v = ç v + v e 3 + v e 3 ÷ s ç a b c ÷ 3 è ø where va, vb and vc are phase voltages. -
The Fundamentals of Ac Electric Induction Motor Design and Application
THE FUNDAMENTALS OF AC ELECTRIC INDUCTION MOTOR DESIGN AND APPLICATION by Edward J. Thornton Electrical Consultant E. I. du Pont de Nemours Houston, Texas and J. Kirk Armintor Senior Account Sales Engineer Rockwell Automation The Woodlands, Texas Edward J. (Ed) Thornton is an Electrical Electrical Mechanical Consultant in the Electrical Technology Coupling System Field System Consulting Group in Engineering at DuPont, in Houston, Texas. His specialty is the design, operation, and maintenance of electric power distribution systems and large motor installations. He has 20 years E , I T , w of consulting experience with DuPont. Mr. Thornton received his B.S. degree Figure 1. Block Representation of Energy Conversion for Motors. (Electrical Engineering, 1978) from Virginia Polytechnic Institute and State University. The coupling magnetic field is key to the operation of electrical He is a registered Professional Engineer in the State of Texas. apparatus such as induction motors. The fundamental laws associated with the relationship between electricity and magnetism were derived from experiments conducted by several key scientists J. Kirk Armintor is a Senior Account in the 1800s. Sales Engineer in the Rockwell Automation Houston District Office, in The Woodlands, Basic Design and Theory of Operation Texas. He has 32 years’ experience with The alternating current (AC) induction motor is one of the most motor applications in the petroleum, rugged and most widely used machines in industry. There are two chemical, paper, and pipeline industries. major components of an AC induction motor. The stationary or He has authored technical papers on motor static component is the stator. The rotating component is the rotor. -
Vector Control of an Induction Motor Based on a DSP
Vector Control of an Induction Motor based on a DSP Master of Science Thesis QIAN CHENG LEI YUAN Department of Energy and Environment Division of Electric Power Engineering CHALMERS UNIVERSITY OF TECHNOLOGY G¨oteborg, Sweden 2011 Vector Control of an Induction Motor based on a DSP QIAN CHENG LEI YUAN Department of Energy and Environment Division of Electric Power Engineering CHALMERS UNIVERSITY OF TECHNOLOGY G¨oteborg, Sweden 2011 Vector Control of an Induction Motor based on a DSP QIAN CHENG LEI YUAN © QIAN CHENG LEI YUAN, 2011. Department of Energy and Environment Division of Electric Power Engineering Chalmers University of Technology SE–412 96 G¨oteborg Sweden Telephone +46 (0)31–772 1000 Chalmers Bibliotek, Reproservice G¨oteborg, Sweden 2011 Vector Control of an Induction Motor based on a DSP QIAN CHENG LEI YUAN Department of Energy and Environment Division of Electric Power Engineering Chalmers University of Technology Abstract In this thesis project, a vector control system for an induction motor is implemented on an evaluation board. By comparing the pros and cons of eight candidates of evaluation boards, the TMS320F28335 DSP Experimenter Kit is selected as the digital controller of the vector control system. Necessary peripheral and interface circuits are built for the signal measurement, the three-phase inverter control and the system protection. These circuits work appropriately except that the conditioning circuit for analog-to-digital con- version contains too much noise. At the stage of the control algorithm design, the designed vector control system is simulated in Matlab/Simulink with both S-function and Simulink blocks. The simulation results meet the design specifications well. -
Abstract Controlling Ac Motor Using Arduino
ABSTRACT CONTROLLING AC MOTOR USING ARDUINO MICROCONTROLLER Nithesh Reddy Nannuri, M.S. Department of Electrical Engineering Northern Illinois University, 2014 Donald S Zinger, Director Space vector modulation (SVM) is a technique used for generating alternating current waveforms to control pulse width modulation signals (PWM). It provides better results of PWM signals compared to other techniques. CORDIC algorithm calculates hyperbolic and trigonometric functions of sine, cosine, magnitude and phase using bit shift, addition and multiplication operations. This thesis implements SVM with Arduino microcontroller using CORDIC algorithm. This algorithm is used to calculate the PWM timing signals which are used to control the motor. Comparison of the time taken to calculate sinusoidal signal using Arduino and CORDIC algorithm was also done. NORTHERN ILLINOIS UNIVERSITY DEKALB, ILLINOIS DECEMBER 2014 CONTROLLING AC MOTOR USING ARDUINO MICROCONTROLLER BY NITHESH REDDY NANNURI ©2014 Nithesh Reddy Nannuri A THESIS SUBMITTED TO THE GRADUATE SCHOOL IN PARTIAL FULFILLMENT OF THE REQUIREMENTS FOR THE DEGREE MASTER OF SCIENCE DEPARTMENT OF ELECTRICAL ENGINEERING Thesis Director: Dr. Donald S Zinger ACKNOWLEDGEMENTS I would like to express my sincere gratitude to Dr. Donald S. Zinger for his continuous support and guidance in this thesis work as well as throughout my graduate study. I would like to thank Dr. Martin Kocanda and Dr. Peng-Yung Woo for serving as members of my thesis committee. I would like to thank my family for their unconditional love, continuous support, enduring patience and inspiring words. Finally, I would like to thank my friends and everyone who has directly or indirectly helped me for their cooperation in completing the thesis. -
Electric Motors
SPECIFICATION GUIDE ELECTRIC MOTORS Motors | Automation | Energy | Transmission & Distribution | Coatings www.weg.net Specification of Electric Motors WEG, which began in 1961 as a small factory of electric motors, has become a leading global supplier of electronic products for different segments. The search for excellence has resulted in the diversification of the business, adding to the electric motors products which provide from power generation to more efficient means of use. This diversification has been a solid foundation for the growth of the company which, for offering more complete solutions, currently serves its customers in a dedicated manner. Even after more than 50 years of history and continued growth, electric motors remain one of WEG’s main products. Aligned with the market, WEG develops its portfolio of products always thinking about the special features of each application. In order to provide the basis for the success of WEG Motors, this simple and objective guide was created to help those who buy, sell and work with such equipment. It brings important information for the operation of various types of motors. Enjoy your reading. Specification of Electric Motors 3 www.weg.net Table of Contents 1. Fundamental Concepts ......................................6 4. Acceleration Characteristics ..........................25 1.1 Electric Motors ...................................................6 4.1 Torque ..............................................................25 1.2 Basic Concepts ..................................................7 -
A DSP Based Servo System Using Permanent Magnet Synchronous
A DSP Based Servo System Using Permanent Magnet Synchronous Motors PMSM Longya Xu, Minghua Fu, and Li Zhen The Ohio State University Department of Electrical Engineering 2015 Neil Avenue Columbus, OH 43210 Abstract- A digital servo system using a Digital Signal Pro cessor DSP is presented in this pap er. A Permanent Magnet Synchronous Motor PMSM with rotor p osition enco der and Hall sensor is used. The eld oriented vector control technique is employed to achieve robust p erformance and fast torque resp onse. The system uses p osition and sp eed regulations as the system outer lo op, and the current regulation with vector control as the inner lo op. A DSP system using TI's TMS320C240 is develop ed, and the prop osed digital control strategy is implemented in the DSP. Key Words: Vector Control, Motion Control, Servo System, Digital Control, Permanent Mag- net Synchronous Motor PMSM, Digital Signal Pro cessor DSP I. Intro duction Precise motion control plays an imp ortant role in various areas such as automation industry, semiconductor industry, etc. Permanent magnet synchronous motors PMSM are ideal for advanced motion control systems for their p otentials of high eciency, high torque to current ratio, and low inertia. Advances in Digital Signal Pro cessors DSP have greatly enhanced the p otential of PMSM in servo applications. Digital control can b e implemented in the DSP, which makes it sup erior to analog based stepp er control, since the controller is much more compact, reliable, and exible. High p erformance of PMSM can be obtained by means of eld oriented vector control, which is only realizable in a digital based system. -
Improvement of Electromagnetic Railgun Barrel Performance and Lifetime By
IMPROVEMENT OF ELECTROMAGNETIC RAILGUN BARREL PERFORMANCE AND LIFETIME BY METHOD OF INTERFACES AND AUGMENTED PROJECTILES A Thesis Presented to the Faculty of California Polytechnic State University San Luis Obispo In Partial Fulfillment of the Requirements for the Degree Master of Science in Aerospace Engineering by Aleksey Pavlov June 2013 c 2013 Aleksey Pavlov ALL RIGHTS RESERVED ii COMMITTEE MEMBERSHIP TITLE: Improvement of Electromagnetic Rail- gun Barrel Performance and Lifetime by Method of Interfaces and Augmented Pro- jectiles AUTHOR: Aleksey Pavlov DATE SUBMITTED: June 2013 COMMITTEE CHAIR: Kira Abercromby, Ph.D., Associate Professor, Aerospace Engineering COMMITTEE MEMBER: Eric Mehiel, Ph.D., Associate Professor, Aerospace Engineering COMMITTEE MEMBER: Vladimir Prodanov, Ph.D., Assistant Professor, Electrical Engineering COMMITTEE MEMBER: Thomas Guttierez, Ph.D., Associate Professor, Physics iii Abstract Improvement of Electromagnetic Railgun Barrel Performance and Lifetime by Method of Interfaces and Augmented Projectiles Aleksey Pavlov Several methods of increasing railgun barrel performance and lifetime are investigated. These include two different barrel-projectile interface coatings: a solid graphite coating and a liquid eutectic indium-gallium alloy coating. These coatings are characterized and their usability in a railgun application is evaluated. A new type of projectile, in which the electrical conductivity varies as a function of position in order to condition current flow, is proposed and simulated with FEA software. The graphite coating was found to measurably reduce the forces of friction inside the bore but was so thin that it did not improve contact. The added contact resistance of the graphite was measured and gauged to not be problematic on larger scale railguns. The liquid metal was found to greatly improve contact and not introduce extra resistance but its hazardous nature and tremendous cost detracted from its usability. -
Field Oriented Control 3-Phase Ac-Motors
Field Orientated Control of 3-Phase AC-Motors Literature Number: BPRA073 Texas Instruments Europe February 1998 IMPORTANT NOTICE Texas Instruments (TI) reserves the right to make changes to its products or to discontinue any semiconductor product or service without notice, and advises its customers to obtain the latest version of relevant information to verify, before placing orders, that the information being relied on is current. TI warrants performance of its semiconductor products and related software to the specifications applicable at the time of sale in accordance with TI's standard warranty. Testing and other quality control techniques are utilized to the extent TI deems necessary to support this warranty. Specific testing of all parameters of each device is not necessarily performed, except those mandated by government requirements. Certain applications using semiconductor products may involve potential risks of death, personal injury, or severe property or environmental damage ("Critical Applications"). TI SEMICONDUCTOR PRODUCTS ARE NOT DESIGNED, INTENDED, AUTHORIZED, OR WARRANTED TO BE SUITABLE FOR USE IN LIFE-SUPPORT APPLICATIONS, DEVICES OR SYSTEMS OR OTHER CRITICAL APPLICATIONS. Inclusion of TI products in such applications is understood to be fully at the risk of the customer. Use of TI products in such applications requires the written approval of an appropriate TI officer. Questions concerning potential risk applications should be directed to TI through a local SC sales office. In order to minimize risks associated with the customer's applications, adequate design and operating safeguards should be provided by the customer to minimize inherent or procedural hazards. TI assumes no liability for applications assistance, customer product design, software performance, or infringement of patents or services described herein. -
Permanent Magnet Servomotor and Induction Motor Considerations
Permanent Magnet Servomotor and Induction Motor Considerations Kollmorgen B-104 PM Brushless Servomotor at 0.4 HP Kollmorgen M-828 PM Brushless Rotor Kollmorgen B-802 PM Brushless Servomotor at 15 HP Kollmorgen B-808 PM Brushless Rotor Permanent Magnet Servomotor and Induction Motor Considerations 1 Lee Stephens, Senior Motion Control Engineer Permanent Magnet Servomotor and Induction Motor Considerations Motion long considered a mainstay of induction motors, encroachment in the area of 50 HP and greater have been seen recently for some applications by permanent magnet (PM) servomotors. These applications usually have dynamic considerations that require position-time closed loop and high accelerations. When accelerating large loads, permanent magnet servomotors can work with very high load to inertia ratios and still maintain performance requirements. Having a lower inertia typically will allow for less permanent magnet motor can result in a greater torque energy wasted within the motor. Torque (τ), is the density than an equivalent induction system. If size product of inertia (j) and rotary acceleration (α). If you matters, then perhaps a system should use one require inertia matching, ½ of your energy is wasted technology over another. Speaking of size, the inertia accelerating the motor alone. If the inertia ratio from ratio can be an important figure of merit should motor to load is large, then control schemes must be dynamic needs arise. If you are going to have high dynamic enough to prevent the larger load from driving accelerations and decelerations, the size of the rotor the motor as opposed to the motor controlling the load. will significantly increase the inertia and decrease the Tradeoffs and knowing what can be negotiated. -
Electromechanical Thrust Vector Control Systems for the Vega-C Launcher
DOI: 10.13009/EUCASS2019-186 8TH EUROPEAN CONFERENCE FOR AERONAUTICS AND SPACE SCIENCES (EUCASS) Electromechanical Thrust Vector Control Systems for the Vega-C launcher Gael Dée *, Tillo Vanthuyne ** , Alessandro Potini ***, Ignasi Pardos ****, Guerric De Crombrugghe ***** * SABCA Haachtsesteenweg 1470, 1130 Brussels. Email: [email protected] ** SABCA Haachtsesteenweg 1470, 1130 Brussels. Email: [email protected] *** AVIO Via degli Esplosivi, 1 Colleferro (RM), Italy. Email: [email protected] **** ESA/ESRIN Largo Galileo Galilei 1, 00044 Frascati, Italy. Email: [email protected] ***** SABCA Haachtsesteenweg 1470, 1130 Brussels. Email: [email protected] Abstract SABCA has designed electrical Thrust Vector Control (TVC) systems for the new VEGA-C launcher stages, based on the experience and lessons learned of the VEGA TVCs in operation since the first VEGA flight in February 2012. The paper presents the main drivers and lessons learned introduced in the design of this new generation of TVC systems. 1. Introduction The VEGA-C launcher, currently under development, is the evolution of the VEGA European launcher. It has been introduced to Increase performances, with a 2200 kg load capacity in LEO (a 700 kg increase with regard to VEGA) Reduce operating costs Reduce dependency on non-European sources Like VEGA, VEGA-C consists of 3 stages based on solid propulsion engines and a 4th stage based on a liquid propulsion engine. The first stage is based on the new P120C solid rocket motor, which is the largest monolithic carbon fibre SRM ever built. The P120C motor is also used as booster for the new Ariane 6 launcher, serving as a common building block for both launchers. -
Hyperloop Accelerator Design Review
Hyperloop Accelerator Design Review TA: Benjamin Cahill ECE 445 February 25, 2015 Mohammad Jaber Michael Eraci Shivam Sharma Group #24 Table of Contents 1.0 Introduction............................................................................................................... 3 1.1 Statement of Purpose................................................................................. 3 1.2 Objectives...................................................................................................... 3 1.2.1 Benefits ........................................................................................... 3 1.2.2 Features .......................................................................................... 3 2.0 Design......................................................................................................................... 4 2.1 Block Diagram .............................................................................................. 4 2.2 Block Descriptions...................................................................................... 5 3.0 Schematics and Simulation .................................................................................. 6 3.1 Circuit Diagram ............................................................................................ 6 3.2 Control Flow Diagram ................................................................................ 7 3.3 Simulations ................................................................................................... 7 4.0 Requirements