A Procedure for Systematic Determination of the Effects of Component-value Changes in Automatic Control Systems |
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Page 20
... error occurring ( 10 ) immediately following the application of the input . Thus , Wescott proposes the use of the integral of time - multiplied squared - error ( 3-5 ) 14 - Soc e2 ( t ) dt ( 3,4,5 ) and Graham and Lathrop multiplied ...
... error occurring ( 10 ) immediately following the application of the input . Thus , Wescott proposes the use of the integral of time - multiplied squared - error ( 3-5 ) 14 - Soc e2 ( t ) dt ( 3,4,5 ) and Graham and Lathrop multiplied ...
Page 22
... squared - error or integral - absolute - error . The integral - squared - error is chosen because of its general use in practice and because of the comparative ease with which it can be accurately calculated analytically . In terms of ...
... squared - error or integral - absolute - error . The integral - squared - error is chosen because of its general use in practice and because of the comparative ease with which it can be accurately calculated analytically . In terms of ...
Page 74
... Squared - Error , I 0.4 0.2 ་་་ ། 6 c 2 5 8 7 6 6 az by 0.5 2 10 20 50 100 200 500 Forward Gain , K Figure 5-7B 10 1.0 0.8 0.6 Integral - Squared - Error , I. 74.
... Squared - Error , I 0.4 0.2 ་་་ ། 6 c 2 5 8 7 6 6 az by 0.5 2 10 20 50 100 200 500 Forward Gain , K Figure 5-7B 10 1.0 0.8 0.6 Integral - Squared - Error , I. 74.
Common terms and phrases
0.8 0.6 Integral-Squared-Error 5-8 inclusive 500 Forward Gain ABD Systems affords analog computer analytic design application approaches infinity BBD Systems Chapter characteristic equation chute mouth Class AAA Systems Class ABD Dashed Curve Data Pertinent decrease the value denominator of G(s desirable determine DOCTOR OF PHILOSOPHY Effect of Changes error Expression 6-3 feedback control system Figure and Curve Figures 5-1 Graham and Lathrop high range inequality in Expression integral indices intermediate range K Figure large values low range numerator of G(s numerical values optimum values output Parameter Values performance index characteristics performance indices performance quality Pertinent to Class phase margin Plot polynomials position control system resulting s-plane s(T₁s step-function input system parameters systems are possible Systems G(s Systems T1 T2 T₁ T2 T3 Figure T₂s Table 5-6b Data Table 5-la thesis time-constant transfer functions transient performance Values of Gain variation yields zero