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Diagram of the control system.

Diagram of the control system.

Source publication
Article
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This paper considers the robust control of an active radial magnetic bearing system, having a homopolar, external rotor topology, which is used to support an annular fiber composite flywheel rim. A first-order dynamical compensator, which uses only position feedback information, is used for control, its design being based on a linearized one-dimens...

Contexts in source publication

Context 1
... dynamical mathematical model for the AMB shown in Fig. 1, can be established as follows: (1) where mass of the rotor (kg); position displacement of the rotor (m); nominal air gap (m); permeability of free space H/m; total pole-face area of each electromagnet (m ); number of turns on each electromagnet coil; electromagnet coil currents (A); an unknown disturbance (N); some known force acting on the rotor (N). When (1) is linearized at the equilibrium point, ie., and augmented with the control structure shown in Fig. 2, the linearized model is obtained as the following second-order system: Due to inaccuracies in the measurement of some of the phys- ical parameters and changing environmental conditions, the system parameters and are generally uncertain. However, without loss of generality, it can be assumed that their values lie within some known intervals where , and are known scalars ...
Context 2
... the dynamical compensator (5) is applied to the orig- inal nonlinear system (1), with a consideration of current satu- ration as in Fig. 2, the closed-loop system is if if if In order to simulate the system, the parameters and and their upper and lower bounds are determined from (2b), based on the parameter values in Table I. In order that the designed controller can tolerate sufficient parameter uncertainties, large intervals for and were chosen. The values of and , and those of the interval boundaries, and , , for both the vertical and horizontal axes, are given in Table II. Choosing , and , the coeffi- cients of the dynamical compensators are obtained as shown in Table ...

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Citations

... The AC homopolar machine is also well-known as the homopolar synchronous machine and the homopolar inductor alternator [85]. The HMs are able to offer encouraging advantages of robust rotor structure, low idling losses, improved reliability, and thus, they are noticeably attractive for long-term high-speed operation, which is essential for great importance in FESSs [85][86][87][88][89][90][91][92][93][94][95][96]. ...
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... In this work, the Wheatstone Bridge (WB) configuration for the AMBs power coil is considered [5]. A wide range of control techniques have been proposed and investigated with the aim to minimize power dissipation [6], improve dynamic response [7] or increase robustness against unknown parameters or disturbances [8]. ...
... The cost functions in (7) represent the tracking errors for each converter leg, where iDC * , ix * and iy * are the current references for the HB 1, 2 and 3 respectively. It is important to highlight that, since the input and output current of each HB are controlled to minimize the error with respect the same current reference, implementing (7) inherently minimize the cost functions in (8). The cost functions in (8) represents the unbalance on each HB currents. ...
... It is important to highlight that, since the input and output current of each HB are controlled to minimize the error with respect the same current reference, implementing (7) inherently minimize the cost functions in (8). The cost functions in (8) represents the unbalance on each HB currents. It can demonstrated that if the cost functions in (8) are kept equal to zero there is no current circulation through the three HBs (i.e. ...
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... vacuum and r actively con to these advan strial applicatio nergy storage f ompressors, et considers a bas t on each side o l on which the a second-ord turbances. The l described by modeled dyna [2]. To elim output feedbac rotor position s rix inequalitie mulation and de problems. ...
... the system (28) can be converted into the following equivalent state-space form: [2] ∆ ∆ ∆ 0 1 0 , ...
... where , , and are four scalar controller coefficients, to be designed, and the term is introduced to compensate for the effect of the force , the coefficient being given by [2]: ...
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