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                                                                                      October 9, 2014 8:1
            JWST499-c06
                        JWST499-Cetinkunt
                                                                                        SENSORS  343  254mm×178mm
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                             FIGURE 6.14: Excitation voltage for the rotor winding and the induced stator voltages. The
                             induced voltages are shown as a function of time for a constant rotor speed over a period of
                             one revolution.


                             angular position changes beyond one revolution are kept track of through digital counting
                             circuits. The rotor excitation voltage is (generated by an oscillator circuit),
                                                         V (t) = V  ⋅ sin(w t)                  (6.53)
                                                          r     ref     r
                             The induced voltage on the stator windings are (Figure 6.14)
                                          V (t) = k ⋅ V (t) ⋅ sin(  (t)) = k ⋅ V  ⋅ sin(w t) ⋅ sin(  (t))  (6.54)
                                           s1     0  r             0   ref    r
                                          V (t) = k ⋅ V (t) ⋅ cos(  (t)) = k ⋅ V  ⋅ sin(w t) ⋅ cos(  (t))  (6.55)
                                           s2     0  r             0   ref     r
                             Next, the V , V are multiplied by sin and cos functions in the RTDC circuit,
                                          s2
                                      s1
                                                  V (t) = k ⋅ V (t) ⋅ sin(  (t)) ⋅ cos(  (t))   (6.56)
                                                          0
                                                             r
                                                   f1
                                                  V (t) = k ⋅ V (t) ⋅ cos(  (t)) ⋅ sin(  (t))   (6.57)
                                                             r
                                                   f2
                                                          0
                             Then the output of the error amplifier is
                                                ΔV (t) = k ⋅ V ref  ⋅ sin(w t) ⋅ sin(  (t) −   (t))  (6.58)
                                                        0
                                                                    r
                                                  f
                             Then, the signal is demodulated to remove the sin(w t) component by a rectifier and low
                                                                        r
                             pass filter. Then, the signal is fed to an integrator which provides input to the voltage
                             controlled oscillator (VCO). The output of the VCO is fed to an up-down counter to keep
                             track of the position. This results in making the up-down counter increase or decrease    in a
                             direction so that sin(   −   ) approaches zero. The value of the up-down counter is converted
                             to angle    by a DAC as an analog signal to feed the sin and cos multiplication circuit. The
                             iteration on    continues until    =   , at which time the rotor position information is latched
                             from the up-down counter as digital data. The algorithm finds the angle    by iteratively
                             changing   . The iteration stops when ΔV is equal to zero, at which time it means that
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