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Industrial Brushless Servomotors Episode 7 ppsx

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Motor and load dynamics 115 13.7 ms. Viscous damping and friction have been ignored and so the decay is the result of i2R loss in the stator winding. m I o:-73,4 -2oo -lo6i -jco 9=317 300 200 100 -100 -200 - 300 -jo~ Figure 4.11 Poles of an unloaded motor with T e ~ 5Tm 4.4 Variation of load inertia Inclusion of a load inertia JL increases the overall mechanical time constant to 7"M - (1 + JL/Jm)Ym The ratio of electrical to mechanical time constant falls from Te/Ym to 7"e/YM. It is of interest to plot the locus of the poles on the s-plane as the ratio changes. The poles appear at the values of s which make the denominator of the transfer function for the motor-load unit equal to zero, that is when 1 1 S 2 I- S }-~ = 0 Ye Te T M Industrial Brushless Servomotors 4.4 116 The roots of the quadratic are S "- - 2-'~e -+ 77.2 TeT M When rM > 4re, there is no sinusoidal component and the two poles lie along the horizontal axis of the s-plane. The physical interpretation of the two rates of exponential decay is that the transient response dies away relatively quickly at first, and then more slowly as time goes on. When rM < 4re the response is partly exponential and partly sinusoidal. The poles appear at s = rr 4-jw = 2re + j e~'M 4r 2 For example, when 7"M = "re, s = ( 0.5 4-jv/3/2)/r~, i.e. at the 60 ~ position. When rM = 4re both poles lie at 1 S O" 2r~ Figure 4.12 shows how the poles move as the ratio JL/Jm rises to make the value of the overall mechanical time constant change from one-fifth to more than four times the value of the electrical time constant. For the example of the unloaded motor with the poles shown in Figure 4.11, this would mean increasing the load inertia from zero to greater than 19Jm. Overshoot Figure 4.13 shows an exponential and oscillatory variation with time of the speed of an initially stationary motor-load unit, following a step input of voltage. We know that 1 cr = and 2re TeT M 41-2 Motor and load dynamics lit 77 ~ 6r 4 \\ \ \ ~.~ -7 0.2% ,/ ' ! ! I I J" i ~, 2r ! 0 Figure 4.12 Movement of poles as load inertia is increased The response is shown as per-unit of a final steady-state speed and has a maximum value during the first overshoot. The per- unit speed at T/2 is 1 + e -~r/2, or 0.,/m = 1 + e -Tr/2wre toss ,/3 When rM Te W 2~re and therefore a3m = 1 + e -r/v/3 = 1.163 (.Uss 1 When TM - 2re w =~ and ZTe = 1 +e -~- 1.043 ~SS This means that the speed overshoot shown in Figure 4.13 increases from about 4% to 16% of a final steady,state speed as the pole position shown in Figure 4.12 is changed from 118 Industrial Brushless Servomotors 4.4 45 ~ to 60 ~ As the pole angle increases, the frequency a; of the oscillatory component also increases and so the time in which ~m reaches the zone of the first overshoot shortens. Reducing the response time in this way is, however, at the expense of increasing both the overshoot and the risk of system instability. I I 2 ,t, L =m i i I I1 i ' . r ~ I ] t I [ tl'c~ "'_' l , ,' ] ' ' ~"'-_" ' i t .= 1 "'= ' 4" : I ' l '. F s" l ~ I I i " " I ' I o T~ I,' ' " - =. . ,, ,, % ~P t , I I z T = 2~o~ , ~l' IP- Figure 4.13 Overshoot of motor speed System control We have studied the transient responses which are taken into account when the motor and load are incorporated into the system as a whole. In practice, the control system is designed to eliminate the voltage step-input poles of the motor-load unit. The motor current is controlled to give the motor and load a relatively rapid change of speed, with less than 5% overshoot. The appearance of a larger than designed overshoot and associated instability is often the result of a load inertia which differs from the value used in the design of the control system. The best results are achieved when the amplifier tuning parameters include the range of inertias of the load masses likely to be driven by a particular motor [5]. Motor and load dynamics 119 4.5 Optimization Understanding the dynamics of the motor and load is particularly important when an application involves incremental motion, where the load is required to move in discrete steps with a specific velocity profile. The steps can be in the form of an angle of rotation of a load driven through a direct or geared shaft coupling with the motor, or in the form of linear translation where the load is moved, for example, by a belt and pulley mechanism. Figure 4.14 shows a handling system used in the manufacture of filters for the automobile industry which allows three-axis translation and also rotation of the loads. The need for rapid rotation or translation often means that a load must be accelerated and decelerated back to rest over a relatively short time. Two main factors are involved in the minimization of the stator i2R loss, and therefore of the required size and cost of a motor. We start by looking at the effect of the profile of the waveform of load velocity against time, and then go on to include the effect of the ratio between the moments of inertia of the motor and load. Figure 4.14 Four-axis handling system. (Photo courtesy of Hauser division of Parker Hannifin) 120 Industrial Brushless Servomotors 4.5 Load velocity profiles Figure 4.15 shows a motor connected to a rotating load through a geared reducer. The inertias Jm and JL are assumed to include the inertias of the shaft and gear on the respective sides of the reducer. Figure 4.16 shows the general trapezoidal load velocity profile, with unequal periods of acceleration, constant speed and deceleration. Here, we are using the trapezoidal term to describe a four-sided figure with two parallel sides. By adding together the angles of rotation during the three periods and equating to the total angle 0p, the constant speed is found to be Op tp[1 0.5(pl +P2)] I~ TL I J~ Figure 4.15 Geared drive: ~m GWL tom t,O L A L/ K For the symmetrical profile of Figure 4.17(a), Pl - P2 - P, and the constant speed of the load is 0p ~0 c tp(1 -p) The rate of acceleration and deceleration of the load in the case of the symmetrical profile is Motor and load dynamics 121 d ~c -dt O'; L p t p Combining the last two equations above and writing WL as a;m/G gives the rate of acceleration and deceleration of the motor as COL d GOp dt wm- t~p(1 - p) 9 p,t~ ~1 I t~ I Figure 4.16 General trapezoidal, velocity profile Stator fiR loss In Figure 4.15, the motor drives a rotating load through a reducer of ratio G. Torque TL is assumed to be constant. If the load velocity is to follow the symmetrical profile of Figure 4.17, the motor torque required during the acceleration and deceleration periods is T- KTi- jdwm + TLG The motor current during the same periods is therefore J d TL i ~ ~~m -~-~ KT dt GKT 122 Industrial Brushless Servomotors 4.5 or i-I~ +I2 where Ii is the component of motor current required for the constant acceleration or deceleration of the load and 12 is the component which provides a constant output torque. Figure 4.17(b) shows the current waveform (rms in the case of the sinusoidal motor). Note that /1 is negative during deceleration. The total energy in joules produced in the form of heat by the iZR loss is e = [p(I2 + II )2 _+. (1 - 2p)I 2 + p(I2 - I1 )2]Rtp (J) = (2pI 2 + I2)Rtp giving e_Rtp d / 2 2] Replacing d wm with the form already found in terms of G, 0p, lit tp and p gives the stator heating energy as P 2 where the profile constant is cp- p(1 -p)2" For a given motor, load, and reducer ratio G, the stator heating is at a minimum when d d 2 e-0, i.e. when dp dp p(1 _p)2 giving =0 1 P-~ The most efficient symmetrical profile is therefore equally distributed, as shown in Figure 4.18. When p- 1/3, the profile constant is Cp - 13.5 Motor and load dynamics 123 The last expression for c above can be shown to apply when the load velocity follows the general trapezoidal profile of Figure 4.16. The profile constant becomes -1 p] + p~-i Cp [1 - 0.5(pl "[-p2)] 2 The constant has a value greater than 13.5 at all relevant values of p] and p2 other than p~ = P2 -1. Stator heating is therefore at a minimum when the trapezoidal profile of load velocity is equally distributed. (b) 03 c CO L (a) 0 ~. ptp ~ (1-2p) tp I1 I I ~L pip .~ I I I I I1-~ I I t Figure 4.17 Motor current for the symmetrical, load velocity profile The second term of the last expression above for c does not depend on Cp, and profile optimization is unnecessary when the load torque requires most of the KTI product. Optimization of the velocity profile can be of benefit if the acceleration and deceleration of the load mass is responsible for a high proportion of the total stator i2R loss. Such cases are likely to arise when a substantial load mass is moved rapidly and repeatedly. 124 Industrial Brushless Servomotors 4.5 CO L i tp 3 o tp t Figure 4.18 %=30p 2tp 2tp = 3 Optimum trapezoidal profile for incremental motion The inertia match for the geared drive When the speed of a load is changed many times per second, backlash in the transmission components can obviously cause problems. Gear reducers used for incremental motion must be of very high quality and are relatively expensive. A planetary reducer with a maximum backlash of 2 to 3 arcminutes may have the same order of price as the drive motor itself. We have already seen how the load velocity profile affects the motor losses, and now follow on by including the effect of the ratio between the inertias of the motor and load masses. The inertial load In Figure 4.15 the load is purely inertial when load torque TL is zero. Ignoring reducer losses, motor friction and viscous damping, the motor torque is given by d T- KTi= J~t m [...]... 126 Industrial B r u s h l e s s S e r v o m o t o r s 4.5 Note that although Go is independent of the velocity profile, the same is not true of the heating energy e However, for any particular combination of motor, inertial load and velocity profile, the energy is a function of the gear ratio alone For reducer ratios G and Go, the energies are JL e 7GZ(Jm + ~_~)2 and co - 7G02(Jm + JL~2 where 7 is... and an output torque, for any trapezoidal velocity profile We have optimized the ratio of a reducer for any trapezoidal velocity profile, and we found earlier that the most efficient 128 4.5 IndustrialBrushless Servomotors shape is equally distributed The trapezoidal profile has the advantage of ease of control by the drive It is not, however, the most efficient velocity profile in general The lowest... loss Minimization of the i2R loss is desirable when a significant part of the stator heating is due to the effect of load and motor inertia on the motor torque requirement Minimization may 130 Industrial Brushless Servomotors 4.5 still be worthwhile when the output load torque forms a relatively high proportion of the total torque, but the optimum gear ratio (and therefore the motor speed) rises with... 0 is the optimum radius of the belt drive pulley when there is no opposing load force, for any velocity profile Working in the same way for the case where F :/: 0 gives rzx - ff v/1 + A2 132 IndustrialBrushless Servomotors 4.5 rA is the optimum pulley radius when the load includes an opposing force, for any trapezoidal velocity profile The inertias of the drive pulley and reducer have so far been ignored... this is that the ball screw may be backdriven by the load if the motor torque is lost, say through a power failure Consequently, the ball screw driving motor must be fitted with a brake 134 Industrial Brushless Servomotors 4.5 In the case of the lead screw, the threads are in direct contact This results in a transmission which is inefficient in comparison to the ball screw, but which does not backdrive... Dividing e by e0 and rearranging gives the extra heating factor for a non-optimum gear ratio as ~=0.25 ( G G~ 2 Go+G ~ _~,,~ ~ < _ 14 1 ,, ! | ! ! | i | ,, ,, 0 .7 1.4 2 3 G -, Go Figure 4.19 Increase in stator heating when G # Go(7L = 0) Ref [4] develops the above expression and plots the energy ratio as the gear ratio falls in comparison to the optimum value The curve has the same shape when... rising values of gear ratio in comparison to the optimum Figure 4.19 shows how the fiR loss increases as the gear ratio deviates from the ideal As a rule of thumb: Motor and load dynamics . that is when 1 1 S 2 I- S }-~ = 0 Ye Te T M Industrial Brushless Servomotors 4.4 116 The roots of the quadratic are S "- - 2-'~e -+ 77 .2 TeT M When rM > 4re, there is no sinusoidal. dynamics 115 13 .7 ms. Viscous damping and friction have been ignored and so the decay is the result of i2R loss in the stator winding. m I o: -73 ,4 -2oo -lo6i -jco 9=3 17 300 200 100. voltage. We know that 1 cr = and 2re TeT M 41-2 Motor and load dynamics lit 77 ~ 6r 4 \ ~.~ -7 0.2% ,/ ' ! ! I I J" i ~, 2r ! 0 Figure 4.12 Movement of

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