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نویسندگان: 

, , ,

نشریه: 

اطلاعات دوره: 
  • سال: 

    1401
  • دوره: 

  • شماره: 

  • صفحات: 

    41-48
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    21
  • دانلود: 

    0
کلیدواژه: 
چکیده: 

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نویسندگان: 

,

نشریه: 

اطلاعات دوره: 
  • سال: 

    1401
  • دوره: 

  • شماره: 

  • صفحات: 

    13-20
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    14
  • دانلود: 

    0
کلیدواژه: 
چکیده: 

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نویسندگان: 

KUMAR P. | Kumar Chaudhary s.

اطلاعات دوره: 
  • سال: 

    2018
  • دوره: 

    31
  • شماره: 

    2 (TRANSACTIONS B: Applications)
  • صفحات: 

    322-330
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    197
  • دانلود: 

    0
چکیده: 

In this paper, a new comparative approach was proposed for reliable Controller design. Scientists and engineers are often confronted with the analysis, design, and synthesis of real-life problems. The first step in such studies is the development of a 'mathematical model' which can be considered as a substitute for the real problem. The mathematical model is used here as a plant. Fractional integrals and derivatives have found wide application in the control of dynamical systems when the controlled system and the Controller are described by a set of fractional order differential equations. Here the stability and robustness of fractional order system is checked at the different level and it is found that the stability region is large in the complex plane. This large stability region provides the more flexibility for system implementation in the control engineering. Generally, an analytically or experimentally approaches are used for designing the Controller. If a fractional order Controller design approach used for a given plant then the controlled parameter gives the better result.

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نویسندگان: 

KUMAR NAVEEN | Ohri Jyoti

اطلاعات دوره: 
  • سال: 

    2020
  • دوره: 

    14
  • شماره: 

    4
  • صفحات: 

    67-74
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    117
  • دانلود: 

    0
چکیده: 

Haptic technology has enormous applications in several fields from medical, military, and in our day-to-day life’ s products including video games, smartphones, and smart cities. The Haptic Interface Controller (HIC), a key circuitry for interaction between the user and the virtual world, has two main control issues: stability and transparency. These two issues are complementary to each other i. e. emphasis on one will degrade the other and vice-versa. To address this, intelligent control techniques including Genetic Algorithm (GA), Feed-Forward Neural Network (FFNN), and Fuzzy Logic Control (FLC) have been used in design of the HIC. To ensure the performance in real-time, in system parametric uncertainty and delay have been added while designing the HIC so that a balance could be maintained between the two issues.

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اطلاعات دوره: 
  • سال: 

    1398
  • دوره: 

    21
  • شماره: 

    1
  • صفحات: 

    151-175
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    477
  • دانلود: 

    193
چکیده: 

مدل سیستم تهویه باید طوری تحلیل شود که تاثیر پارامترهای کنترلی، راحتی انسان در کابین را فراهم کند. در حالی که معمولا از مدل ساده شده معادلات حالت استفاده می شود در این مقاله ضمن بهره گیری از فرم پارامتری معادلات دینامیکی در شبیه سازی ها، براساس تئوری کنترل پیشرفته و روش پیش بین اقدام به انتخاب بهترین ورودیها برای سیستم در نقاط کاری بااستفاده از الگوریتم ژنتیک شده وکنترل کننده ای طراحی خواهد شد که ضمن داشتن کمترین خطای حالت ماندگار در کنترل دمای کابین، پاسخ سریع سیستم وکاهش تاثیر اغتشاش، باعث به حداقل رساندن مصرف انرژی نیز می گردد.

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اطلاعات دوره: 
  • سال: 

    1386
  • دوره: 

    5
  • شماره: 

    4
  • صفحات: 

    203-214
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    1119
  • دانلود: 

    296
چکیده: 

در این مقاله، روشی برای کنترل مقاوم سیستم های حرکت از راه دور ارایه می شود. در این روش، با استفاده از ایده پیش بین اسمیت، یک کنترل کننده امپدانس برای ربات فرمانده و یک کنترل کننده معکوس تطبیقی برای ربات فرمانبر به گونه ای طراحی می شوند که تاثیر حاصل از تاخیر زمانی کانال های مخابراتی بر روی پایداری و کارآیی سیستم حلقه بسته حذف شود. همچنین، شرایطی به منظور حصول پایداری عملی سیستم بر اساس نظریه کنترل مقاوم به دست آورده می شوند. ویژگی های مطلوب در پاسخ گذرای سیستم نیز با استفاده از روش چندجمله ای های مشخصه استاندارد در طراحی گنجانده می شوند. از مزیت های روش پیشنهادی می توان به تعدیل نمودن محدودیت های حاکم بر پیش بین اسمیت، عدم ضرورت اطلاع دقیق از مدل سیستم فرمانده و حصول کارآیی سیستم حلقه بسته در تعقیب موقعیت اشاره کرد. همچنین، روش پیشنهادی با روش غیرخطی مود لغزشی مقایسه می شود. نتایج حاصل از شبیه سازی نشان می دهند که روش پیشنهادی از بازدهی خوبی برخوردار است.

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نویسندگان: 

ALFI ALIREZA

اطلاعات دوره: 
  • سال: 

    2016
  • دوره: 

    5
  • شماره: 

    1
  • صفحات: 

    1-11
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    223
  • دانلود: 

    0
چکیده: 

In this paper, Teaching-Learning-Based Optimization (TLBO) algorithm is employed for controlling the speed of induction motors using fuzzy sliding mode Controller. The proposed control scheme formulates the design of the Controller as an optimization problem. First, a sliding mode speed Controller with an integral switching surface is designed, in which the acceleration information for speed control is not required. In this case, the upper bound of the lumped uncertainties including the parameter uncertainties and the load disturbance must be available. The importance of this parameter on the system performance is illustrated. Then, the fuzzy sliding mode speed Controller is designed to estimate the upper bound of the lumped uncertainties. Finally, TLBO algorithm is adopted to determine the optimal upper bound of the uncertainty. Simulation results are given to demonstrate the superiority of the proposed Controller in comparison with the proportional-integrator, traditional sliding mode Controller, fuzzy sliding mode Controller and adaptive fuzzy sliding mode Controller.

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بازدید 223

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اطلاعات دوره: 
  • سال: 

    1403
  • دوره: 

    13
  • شماره: 

    25
  • صفحات: 

    50-64
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    15
  • 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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نویسندگان: 

MOHAMMADIAN M.

اطلاعات دوره: 
  • سال: 

    2019
  • دوره: 

    7
  • شماره: 

    2
  • صفحات: 

    213-220
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    183
  • دانلود: 

    0
چکیده: 

Background and Objectives: Regulation of protein expression in cellular level are so challenging. In cellular scale, biochemical processes are intrinsically noisy and many convenient Controllers aren’ t physically implementable. Methods: In this paper, we consider standard Lyapunov function and by using Ito formula and stochastic analysis, we derive sufficient conditions for noise to state stability presented in the form of matrix inequalities. In the next step, by defining appropriate change of variables, matrix inequalities are transformed to Linear matrix inequalities which can be used to synthesize Controller with the desired structure. Results: This paper deals with the design of implementable Controller for stochastic gene regulatory networks with multiplicative and additive noises. In particular, we consider structural limitations that are present in real cellular systems and design the decentralized feedback that guarantees noise to state stability. Since the proposed conditions for Controller design are in the form of linear matrix inequalities, Controller gains can be derived efficiently through solving presented LMIs numerically. It is noteworthy that Because of its simple structure, the proposed Controller can be implemented universally in many cells. Moreover, we consider a synthetic gene regulatory networks and investigate the effectiveness of the proposed Controller by simulations. Conclusion: Our results provide a new method for designing Decentralized Controller in gene regulatory networks with intrinsic and extrinsic noises. the proposed Controller can be easily implemented in cellular environment.

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نویسندگان: 

HAMIDI BEHESHTI M.T. | AHVAZI A.

اطلاعات دوره: 
  • سال: 

    2004
  • دوره: 

    -
  • شماره: 

    16
  • صفحات: 

    1-22
تعامل: 
  • استنادات: 

    0
  • بازدید: 

    305
  • دانلود: 

    0
چکیده: 

In this paper, we try to use modeling based on singular perturbation theory, in order to control satellite attitude during the wide rolling angle maneuvering through nonlinear H∞ control strategy. Differential equations describing dynamics of the satellite are presented first, and by choosing the appropriate dynamic model for actuators and based on the standard singular perturbation model, the closed-loop system is created. Next, this model is put into the appropriate form to solve H∞ problem. Then, after solving the HJI equation, the control law is determined. Simulation results for a nominal satellite control based on our approach are finally presented.

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بازدید 305

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