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Writer: 

Gazor M. | Sadri N.

Issue Info: 
  • Year: 

    2016
  • Volume: 

    47
Measures: 
  • Views: 

    131
  • Downloads: 

    64
Abstract: 

FEEDBACK AND INPUT-STATE LINEARIZATION ARE TWO OF THE MOST IMPORTANT METHODS OF CONTROL LAW DESIGNS. THE MAIN IDEA IN FEEDBACK LINEARIZATION IS TO TRANSFORM A NONLINEAR SYSTEM INTO A LINEAR SYSTEM AND THEN USE THE METHODS OF LINEAR CONTROL THEORY FOR CONTROL DESIGN. THE INPUT-STATE LINEARIZATION IS DESIGNED FOR THE CASES THAT THE SYSTEM IS NOT IN THE CANONICAL FORMS. IN THIS PAPER WE RECALL THESE METHODS AND SHOW HOW THESE MAY BE APPLIED ON SINGULAR DIFFERENTIAL SYSTEMS. IN OUR TALK WE WILL DESCRIBE HOW THESE COMMON METHODS OF CONTROLLER DESIGNS ARE RELATED TO AND ARE DIFFERENT FROM OUR RECENT RESEARCH RESULTS IN BIFURCATION CONTROL.

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Author(s): 

GALLEGOS J.

Journal: 

DYNAMICS AND CONTROL

Issue Info: 
  • Year: 

    1994
  • Volume: 

    4
  • Issue: 

    3
  • Pages: 

    277-298
Measures: 
  • Citations: 

    1
  • Views: 

    84
  • Downloads: 

    0
Keywords: 
Abstract: 

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Issue Info: 
  • Year: 

    2004
  • Volume: 

    1
  • Issue: 

    1
  • Pages: 

    29-46
Measures: 
  • Citations: 

    0
  • Views: 

    318
  • Downloads: 

    178
Abstract: 

Distillation column control has been a challenging problem for numerous research activities. Review of past research reveals that among the advanced control methods applied to this system, little attention has been paid to FEEDBACK LINEARIZATION, even in absolutely theoretical cases. This is due to the singularity of the system in steady-state, which invalidates the linearized control law. In this paper, to overcome this problem, a new idea has been suggested that is based on approximate FEEDBACK LINEARIZATION. Based on this idea, an approximate non-linear model has been introduced for the distillation column which can exactly be linearized while reserving the structural properties of the basic system. The control law is derived from the approximate model and then applied to the basic system. The introduced error between the approximate and basic systems is then fed back by two single loop PID controllers to improve the performance of the system. Further, in these approach disturbances due to changes of feed flow and composition has been perfectly decoupled using the disturbance decoupling theory.

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Issue Info: 
  • Year: 

    2017
  • Volume: 

    16
Measures: 
  • Views: 

    152
  • Downloads: 

    154
Abstract: 

UNMANNED AERIAL VEHICLES (UAVS) ARE BEING USED MORE OFTEN FOR MILITARY AND CIVILIAN PURPOSES SUCH AS TRAFFIC MONITORING, PATROLLING FOR FOREST FIRES, SURVEILLANCE, AND RESCUE, IN WHICH RISKS TO PILOTS ARE OFTEN HIGH. ROTORCRAFT HAVE AN EVIDENT ADVANTAGE OVER FIXED-WING AIRCRAFT FOR VARIOUS APPLICATIONS BECAUSE OF THEIR VERTICAL LANDING/TAKE-OFF CAPABILITY AND PAYLOAD. AMONG THE ROTORCRAFT, QUADROTOR CAN USUALLY AFFORD A LARGER PAYLOAD THAN CONVENTIONAL HELICOPTERS DUE TO FOUR ROTORS. DESIGNING AUTO PILOT WITH THE AIM OF DOING AUTONOMOUSLY THE DESIRED MISSIONS CAN BE INTRODUCED AS AN IMPORTANT FIELD OF QUADROTORS INVESTIGATIONS. IN THIS WORK, TRAJECTORY TRACKING OF A QUADROTOR UAV IS OBTAINED BY CONTROLLING ATTITUDE AND POSITION. WHERE, THE FEEDBACK LINEARIZATION METHOD IS USED. AS A FIRST STEP, NONLINEAR 6 DOF DYNAMIC MODEL OF QUADROTOR IS PRESENTED. THEN, FEEDBACK LINEARIZATION (FBL) METHOD IS UTILIZED FOR REDEFINING THE LINEARIZED DYNAMIC MODEL. THEN, WITH THE AIM OF BEING CAPABLE TO STABILIZE AND TRACK THE DESIRED PATH TRAJECTORIES, AN INVERSE DYNAMIC CONTROLLER IS PROPOSED. AT LAST, A MISSION IS DESIGNED AND SIMULATED TO PROPOSE THE APPLICATION RATE OF DESIGNED CONTROLLER.

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Issue Info: 
  • Year: 

    2006
  • Volume: 

    -
  • Issue: 

    -
  • Pages: 

    207-212
Measures: 
  • Citations: 

    1
  • Views: 

    146
  • Downloads: 

    0
Keywords: 
Abstract: 

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

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Issue Info: 
  • Year: 

    2015
  • Volume: 

    8
  • Issue: 

    3
  • Pages: 

    59-66
Measures: 
  • Citations: 

    0
  • Views: 

    522
  • Downloads: 

    294
Abstract: 

In this study, FEEDBACK LINEARIZATION (FL) for 6R manipulator is designed, simulated and implemented. The presented input-output FL controller has achieved the desired performance for the complicated nonlinear terms in the arm‟s dynamic equations. Simulations were used to test the performance of the controller for point-to-point motion as well as continuous trajectory. The results of the point-to-point motion simulations and experiments were compared, where it indicates that the proposed approach preserved smooth motion in a very short process time with good accuracy. The dynamic load carrying capacity (DLCC), which is a criterion to determine FL controller performance on 6R robot, is also investigated, based on saturated torque of the motors and allowable error bounds. Moreover, it was shown that the control law is able to accurately represent closed-loop equations and simultaneously imposed desirable behavior on 6R robot.

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Author(s): 

Mokhtari M.Abolfazl

Issue Info: 
  • Year: 

    2021
  • Volume: 

    23
  • Issue: 

    1
  • Pages: 

    110-129
Measures: 
  • Citations: 

    0
  • Views: 

    122
  • Downloads: 

    0
Abstract: 

Quadrotor is an underactuated and nonlinear coupled system. in this paper for controlling the dynamic of the system, FEEDBACK LINEARIZATION (FL) method is used to convert the nonlinear model to a simple linear one. Moreover, a combination of fractional order PID (FOPID) with FL is used to improve the tracking ability. Tuning the parameters of NFOPID, because of two more orders of integral and derivation is a complicated task,therefore neural networks (NNs) method is used to cope with this duty. Back propagation (BP) algorithm is used to train the weights of the NNs. Because of the flexibility and online learning of the NNs, the proposed controller can be robust against uncertainties and disturbances. The fractional order operator has infinite dimension and for practical implementation modified Oustaloup's method is used in this paper. and finally the results of the simulations also validate the effectiveness and robustness of the proposed scheme.

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Issue Info: 
  • Year: 

    2007
  • Volume: 

    31
  • Issue: 

    B6
  • Pages: 

    651-662
Measures: 
  • Citations: 

    0
  • Views: 

    1123
  • Downloads: 

    172
Abstract: 

Based on the wavelet transform and fuzzy set theory, we present a fuzzy' wavelet network (FWN) for approximating FEEDBACK LINEARIZATION control input. Each fuzzy rule corresponds to a sub-wavelet neural network (sub-WNN) consisting of wavelets with a specified dilation value. The degree of contribution of each sub-WNN can be controlled flexibly. The constructed rules used to approximate the control signal in which the mathematical model of the system under control is unknown can be adjusted by learning the translation parameters of the selected wavelets and determining the shape of Gaussian membership functions of a fuzzy system. The proposed FWN shows good approximation accuracy and fast convergence. Finally a nonlinear inverted pendulum system is applied to verify the effectiveness and ability of the proposed network.

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Issue Info: 
  • Year: 

    2020
  • Volume: 

    9
  • Issue: 

    4
  • Pages: 

    169-173
Measures: 
  • Citations: 

    0
  • Views: 

    73
  • Downloads: 

    6
Abstract: 

In this paper, a combination of step-back theories and linear FEEDBACK is used to control the status of a satellite. Dynamic equations govern the status of nonlinear and multi-input-multi-output satellites. The angles of rotation, the direction and top of the outputs of this system and the torques around the three axes of the satellite are its inputs. In the proposed algorithm, which uses the step-back theory, in the first step, the linear input-output FEEDBACK method is used for multi-inputmulti-output systems, and the desired angular velocities around the three axes of the satellite are determined. Using this method, in the second step, we will face three single-input-single-output subsystems. Then, in the second step, in order for the angular velocities to reach the desired values, the linear FEEDBACK theory is once again used to generate torques around three axes. Finally, computer simulation is performed to evaluate the efficiency of the proposed method.

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Issue Info: 
  • Year: 

    2018
  • Volume: 

    8
  • Issue: 

    4
  • Pages: 

    2826-2832
Measures: 
  • Citations: 

    0
  • Views: 

    164
  • Downloads: 

    96
Abstract: 

In cruise control systems, the performance of the controller is important. Hence, in order to have accurate results, the nonlinear behavior of a vehicle model should also be considered. In this article, a vehicle with a nonlinear model is controlled by using a nonlinear method. The nonlinear term of the model is the generated torque of engine, which is a polynomial equation. In addition, FEEDBACK LINEARIZATION is used as a nonlinear method in order to design two parallel controllers to control the movement of the vehicle. These two parallel controllers are used to control braking and gas pedals which are in charge of the angular velocity of the wheels. To check the performances of controllers, first, each controller is used separately. Finally, two parallel controllers are used to track the reference signal. Comparison between results shows that the designed controller is able to reduce the convergence time of about 10 seconds. This improvement is near 35% in comparison with near studies. In addition, it can reduce the error between the velocity of the vehicle and the values of the reference signal that results in more safety for passengers.

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