In time delay control systems, the observed information is related to a past instant and using this delayed signal may cause unsatisfactory results in control system applications. This paper deals with how time delay ...
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ISBN:
(纸本)0889866104
In time delay control systems, the observed information is related to a past instant and using this delayed signal may cause unsatisfactory results in control system applications. This paper deals with how time delay information can be used in reorganizing the rule base so as to improve system performance. Basically, it proposes a new scheme of appropriate shifting of the rule base to compensate the information lag caused by time delay in the system. The parameters affecting the shifting scheme are discussed in detail and the shifting scheme is tabulated with respect to system model parameters. Applications of the new methodology in different systems are simulated and the effectiveness of the scheme is fully illustrated.
Panel methods can be widely used in linear aerodynamics (covering inviscid, incompressible and irrotational flow fields), because they give relatively accurate results in acceptable computational time. So, several met...
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ISBN:
(纸本)9789634209683
Panel methods can be widely used in linear aerodynamics (covering inviscid, incompressible and irrotational flow fields), because they give relatively accurate results in acceptable computational time. So, several methods had been developed in this field. One of the methods is the so-called vortex-lattice method. This method is relatively simple;however, it has a stable solution and gives results comparable with wind tunnel tests for conventional wing configurations. Hence it is worth dealing with the improvement of the method. In this lecture possible improvements are developed and tested, which could speed up the solution of the problem, or improve the accuracy of the solution. First of all, the possible arrangement of vortex rings on the wing's camber surface was examined, to the literature it is recommended to place the leading segment of the vortex ring on the panel's quarter chord line and place the collocation point at the centre of the three-quarter chord line. However, if one places the vortex Ime segments on the bounds and the collocation point in the centre of the panel element, only the panel comer points have to be stored, instead of both the panel and the vortex-lattice comer points. Unfortunately the resulting pressure distribution along the wing chord is greatly affected by the vortex ring placement and the method proposed in the literature is more accurate, consequently that method should be used, to the second step, the formulas used for influence coefficient calculations can be improved to speed up the solution. The formula used to calculate the effect of a semi infinite vortex line was simplified, and far field formulas were tested. The simplified formula was faster, but no exact condition was found when far field formulas can be used. In the third step, the influence coefficients can be calculated, considering the neighbouring vortex line segments only once. This was solved by the stepping of an 8 point scheme on the vortex lattice. It needed mo
In this paper, a modified version of the Chaos Shift Keying (CSK) scheme for secure encryption and decryption of data is proposed. The proposed scheme uses the effect of anti-synchronization, rather than synchronizati...
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Robots are complex mechatronics systems where several electric drives are employed to control the movement of articulated structures. In industrial environments they must perform tasks with rapidity and accuracy in or...
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The main objective of this paper is to develop a simulator for powered wheelchair which permits to implement different control and motion planning strategies in order to study their performance and to compare them. In...
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The main objective of this paper is to develop a simulator for powered wheelchair which permits to implement different control and motion planning strategies in order to study their performance and to compare them. In simulation the wheelchair can easily be integrated in any desired environment and the algorithm under test can be implemented and tested in this virtual environment. The paper presents firstly a brief description of a general powered wheelchair, then a control algorithm for a powered wheelchair is discussed based on the position of the wheelchair rather than its velocities. A general algorithm for motion planning and obstacle avoidance is briefly talked. This algorithm calculates the next desired position based on the actual and desired final position of the wheelchair and the obstacle position, motion direction and velocity. The next desired position is then fed to the control unit which executes the command. Some simulation results will be finally presented based on existing techniques like the virtual force field technique and the vector field histogram method
Nonlinear control systems are more difficult to handle than linear, since the associativity is not valid. Laplace transforms and transfer functions, which form a symbolic computation for linear systems, are, therefore...
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Nonlinear control systems are more difficult to handle than linear, since the associativity is not valid. Laplace transforms and transfer functions, which form a symbolic computation for linear systems, are, therefore, disabled. A modern development of nonlinear control systems is thus related mainly to the systematic use of differential algebraic methods. However, such methods allow us to introduce similar symbolic computation also for nonlinear systems. To provide a basis for such a symbolic computation the theory of non-commutative polynomials over the field of meromorphic functions is introduced. In that respect, differential operators, which act on one-forms, play a key role. They form the left skew polynomial ring. Quotients of such polynomials stand for transfer functions of nonlinear systems. In other words, presented paper tries to show that there is no reason to believe well known dogma saying that nonlinear systems have no transfer functions
The problem of design of a controller for a large-scale system is studied. The design objective is to achieve behavior comparable with the standard controller that is LQ optimal. On the other hand the amount of interc...
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ISBN:
(纸本)9783902661159
The problem of design of a controller for a large-scale system is studied. The design objective is to achieve behavior comparable with the standard controller that is LQ optimal. On the other hand the amount of interconnections between subsystems should be kept as small as possible. This is guaranteed by solving of an optimization problem where the number of interconnections is minimized while the difference in the values of the cost functional for the standard and decentralized controller is a constraint. To find the value of the cost of the decentralized control in presence of interconnections one can use linear matrix inequalities.
This paper presents the Model Predictive controller design process when an unknown input observer provides measured disturbance form unmeasured one. Instead of using an unmeasured disturbance dynamic implemented into ...
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Underwater vehicles are highly nonlinear and complex systems, that makes designing autopilots extremely difficult. This paper presents autotuning as a method for tuning parameters of a micro-ROV autopilot. The main be...
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Underwater vehicles are highly nonlinear and complex systems, that makes designing autopilots extremely difficult. This paper presents autotuning as a method for tuning parameters of a micro-ROV autopilot. The main benefit of this procedure is that the model of the process does not have to be known. Autotuning is often used for industrial processes but not on marine vessels. This procedure, which is performed in closed-loop, is completely automated and enables the operator to retune an autopilot whenever ROV performance is degraded (due to different operating points, tether influence, currents, etc.). In this article we use already known different autotuning recommendations (primarily designed for type 0 processes) with some modifications which we recommend for micro-ROVs. We also give results of using different types of PID controllers, whose parameters are being tuned. A real life demonstration on a VideoRay Pro II micro-ROV is provided
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