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متن کامل


اطلاعات دوره: 
  • سال: 

    2016
  • دوره: 

    2
تعامل: 
  • بازدید: 

    349
  • دانلود: 

    0
چکیده: 

PERMANENT MAGNET SYNCHRONOUS MOTOR (PMSM) HAS GAINED MORE INTEREST RECENTLY IN INDUSTRIAL APPLICATIONS. DIGITAL HARDWARE SOLUTIONS SUCH AS FIELD PROGRAMMABLE GATE ARRAYS (FPGAS) ARE THE MOST PREFERRED METHODS FOR CONTROLLING PMSM DRIVERS. THIS PAPER PRESENTS AN IMPLEMENTATION OF A Current CONTROL SYSTEM FOR PMSM BASED ON FPGA. ENCODER-BASED SPEED AND POSITION DETECTION METHOD HAS BEEN USED IN PROPOSED HARDWARE. THE WHOLE SYSTEM HAS BEEN MODELED AND SIMULATED IN SYSTEM LEVEL USING MATLAB/SIMULINK. HARDWARE ARCHITECTURE FOR ALL COMPUTATIONAL BLOCKS IS IMPLEMENTED USING VERILOG HDL. THE HARDWARE ARCHITECTURE HAS BEEN SUCCESSFULLY SYNTHESIZED AND IMPLEMENTED ON ALTERA CYCLONE II FPGA. PROPOSED SYSTEM ARCHITECTURE AND COMPUTATIONAL BLOCKS ARE DESCRIBED AND SYSTEM LEVEL AND RTL SIMULATION RESULTS ARE PRESENTED. SIMULATION RESULTS SHOW THAT THE TOTAL COMPUTATION CYCLE TIME OF IMPLEMENTED SYSTEM ON ALTERA CYCLONE II FPGA IS 456NS.

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بازدید 349

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اطلاعات دوره: 
  • سال: 

    1403
  • دوره: 

    13
  • شماره: 

    25
  • صفحات: 

    50-64
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    16
  • دانلود: 

    0
چکیده: 

The body freedom flutter phenomenon is one of the aeroelastic instabilities that occurs due to the coupling of the aeroelastic bending mode of the wing with the short-period mode in the flight dynamics of the aircraft. By using the aeroservoelastic model and applying closed loop control, this phenomenon can be suppressed in the operating conditions of the aircraft and the velocity of this event can be increased. The simplest model aircraft capable of displaying this instability includes the flexible wing and the planar flight dynamics model. For this purpose, the wing structure is modeled using the Euler-Bernoulli beam and, the theory of minimum variable state is used to model unstable aerodynamics to make the conditions suitable for modeling the system in state space. In the control section, the elevator is used as the control surface and LQR theory with Kalman filter is used to body freedom flutter suppression. Finally, the effect of adding a closed loop control to increase the body freedom flutter velocity and the limitations of this work are studied.

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بازدید 16

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نویسندگان: 

GHADRI SABER | JAVADI SHAHRAM | FAROKHI FARDAD

اطلاعات دوره: 
  • سال: 

    2013
  • دوره: 

    2
  • شماره: 

    2
  • صفحات: 

    91-94
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    324
  • دانلود: 

    0
چکیده: 

Today, DC motors is still being used globally due to their easy speed controllability. In this article, an Adaptive Neuro-Fuzzy Inference System (ANFIS) controller is designed for DC motors. The main purpose of performing such task is to reduce the DC motor starting Current and deleting the ripple Current during starting time in considering control parameters such as: rise time, settling time, maximum overshoot and system steady state error. The results have been simulated in MATLAB and a comparison is made between ANFIS controller and PID controller.

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بازدید 324

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مرکز اطلاعات علمی Scientific Information Database (SID) - Trusted Source for Research and Academic Resources
نویسنده: 

Abolhasani Jabali Mohammad Bagher | Kazemi Mohammad Hossein | Nazarzadeh Jalal

اطلاعات دوره: 
  • سال: 

    2013
  • دوره: 

    1
تعامل: 
  • بازدید: 

    121
  • دانلود: 

    0
چکیده: 

IN IRAN POWER NETWORK ESPECIALLY IN TEHRAN REGIONAL ELECTRIC COMPANY LIKE OTHER POWER SYSTEMS, SHORT-CIRCUIT Current INCREASES BY EXTENSION OF THE ELECTRICAL POWER SYSTEM BECAUSE OF RISING DEMAND OF ELECTRICAL POWER. THIS FAULT Current MAGNITUDE IS MORE THAN THE CIRCUIT BREAKER INTERRUPTING RATINGS ESPECIALLY IN MONTAZERQAEM POWER PLANT. FAULT CurrentS HAVE A GREAT INFLUENCE ON POWER SYSTEM. FOR REDUCING THESE RISKS, SOME EXPENSIVE OR COMPLICATED SOLUTIONS ARE PROPOSED BASED ON INCREASING THE IMPEDANCE OF POWER NETWORK LIKE FCLS OR SERIES REACTORS OR SPLIT BUS. THE APPROACH OF THIS PAPER IS CONTROLLING THE SOURCES OF THE FAULTS. IT PROPOSES A NEW SOLUTION FOR REDUCTION OF THE FAULT Current BY A controller. THE controller IS DESIGNED BY H ¥ MIXED-SENSITIVITY MINIMIZATION METHOD TO CONTROL THE FAULT Current THROUGH CONTROLLING THE FIELD Current OF THE GENERATOR.THIS METHOD IS SIMULATED ON A GENERATOR UNIT WHICH ITS EXCITER SYSTEM IS CONSIDERED FOR MODELING AND CONTROL DESIGN. THE RESULTS SHOW THAT THIS ECONOMICAL SOLUTION IS EFFICIENT ENOUGH.

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بازدید 121

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نشریه: 

Scientia Iranica

اطلاعات دوره: 
  • سال: 

    2022
  • دوره: 

    29
  • شماره: 

    6 (Transactions D: Computer Science and Engineering and Electrical Engineering)
  • صفحات: 

    3288-3303
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    14
  • دانلود: 

    0
چکیده: 

Parabolic carrier PWM method is considered as one of the direct Current control methods which has been proposed for the voltage-source converters (VSCs). This method has an excellent dynamic response. Besides, it proposes a constant switching frequency by employing a pair of parabolic PWM carriers. However, it suffers from some drawbacks and limitations. The major drawback of this method is its sensitivity to the inductance variations. In other words, in grid-connected applications the exact value of grid inductance should be exactly known to achieve a proper performance from this method. Moreover, it is essential that during each switching cycle the voltage at the point of common coupling remains constant. In grid connected applications such as active power filter these drawbacks may lead to operate at variable or non-expected frequencies. Therefore, this paper concerns the suggestions to deal with the situation. In this paper, by applying the conventional method the aforementioned problems are examined in a grid-connected active power filter. It is shown analytically that by using the proposed method, problems of sensitivity to inductance changes and also necessity to constant voltage at point of common coupling in a switching period will be solved. Finally, simulation and experimental results are presented.

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نویسندگان: 

RYAN M.J. | LORENZ R.D.

اطلاعات دوره: 
  • سال: 

    1995
  • دوره: 

    -
  • شماره: 

    -
  • صفحات: 

    507-513
تعامل: 
  • استنادات: 

    1
  • بازدید: 

    132
  • دانلود: 

    0
کلیدواژه: 
چکیده: 

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بازدید 132

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نویسندگان: 

, , ,

نشریه: 

اطلاعات دوره: 
  • سال: 

    1401
  • دوره: 

  • شماره: 

  • صفحات: 

    41-48
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    24
  • دانلود: 

    0
کلیدواژه: 
چکیده: 

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بازدید 24

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اطلاعات دوره: 
  • سال: 

    1395
  • دوره: 

    1
تعامل: 
  • بازدید: 

    565
  • دانلود: 

    283
چکیده: 

این پژوهش بر اساس تحلیل دینامیکی جریان گاز در داخل یک سانتریفیوژگازی بلند با استفاده از شرایط مرزی می باشد. در این پروژه ما بر پایه روش تفاضل محدود، با استفاده از کد برنامه نویسی Fortran و روش تکرار گوس سایدل و ژاکوبی و بر اساس نوع مش بندی مربعی با نقاط ثابت و دستگاه معادلات بقایی، 4 معادله غیر خطی بیضوی، تابع جریان، حالت گردابی، انرژی وسرعت Azimuthal و معادلات دیگر را تحلیل نمودیم. در این مقاله نوع مش بندی روتور از نوع متناوب بوده که 50 نقاط گرهی در راستای شعاعی و 100 نقاط گرهی در راستای محوری می باشد وهمچنین در این مش بندی مبحث مهم Claustering در مناطق مختلف روتور رعایت شده است. از طرفی خواص حرارتی دیواره سیلندر و کلاهک های انتهایی و همچنین ضریب انتقال حرارت بین سیلندر دوار و محیط اطراف اثر بسیار محدودی بر روی عملکرد جداسازی در یک سانتریفیوژ گازی بلند دارد.

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اطلاعات دوره: 
  • سال: 

    1391
  • دوره: 

    19
تعامل: 
  • بازدید: 

    473
  • دانلود: 

    375
کلیدواژه: 
چکیده: 

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اطلاعات دوره: 
  • سال: 

    1395
  • دوره: 

    24
تعامل: 
  • بازدید: 

    365
  • دانلود: 

    341
چکیده: 

لطفا برای مشاهده چکیده به متن کامل (PDF) مراجعه فرمایید.

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