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SYSTEM DYNAMICS & POLE LOCATIONS:

Consider the system shown below:

Assume the system is in equilibrium and is then disturbed

The resulting second order differential equation for the system,

representing the mass displacement from rest, to a step input has a time domain solution given by:

y (t) = 1 - (e--z*ω*t)*Sin( ω*√(1 - z*z)*t +Arc Cos(z) ) / √(1 - z*z)
bulletz = 0.1 =  low damped system many oscillations in (green) output
bulletz = 1 =  high damped system no oscillations in (purple) output

What does changing the value of  z mean with respect to the pole positions of the system. As the value of damping z decreases the position of the pole approaches the imaginary axis. 
bullet The concentric circles represent a constant frequency as damping is varied.
bulletThe radial lines represent constant damping as frequency is varied

 

Transient Response (time domain) of systems to a step disturbance:

A first order system - the time constant of the system is calculated by reading off the time where the output reaches 63% of its final value.

For a second order system several parameters are used to specify the response characteristics:
bulletRise Time: the time difference between 10% and 90% output amplitude values
bulletPeak Amplitude: the magnitude of the maximum overshoot seen in the response
bulletusually given as a % or a gain in dB
bulletSettling Time: the time for the output amplitude to remain within some predefined tolerance limits
bullettypically these limits are +/- 2%, 5%, 10% of the steady state value

Calculations used for time response characteristics:

 
ωn = ωo natural frequency
 

Note:

ωn = 2*π*fn Rise time Peak Time
(p - b)/ωd
ζ damped frequency ωd b σ Tr Tp Mp = M Ts 2% Ts 5% Mr = Mp ωr ωb ωc ωo*Tr ωbo ωco Φm
[Hz] arctan(ωd/σ) ζ*ωn [s] [s] % [s] [s] [dB] [Hz] [Hz] [Hz] deg
0.001 1 1.569796327 0.001 1.5718 3.1416 100% 4000 3000 53.9794 1 1.5538 1 1.5718 1.5538 1 0.11581
0.1 0.99499 1.470628906 0.1 1.67938 3.1574 73% 40 30 14.02305 0.98995 1.5428 0.9901 1.67938 1.5428 0.9901 11.4217
0.2 0.9798 1.369438406 0.2 1.8087 3.2064 53% 20 15 8.136088 0.95917 1.5096 0.9608 1.8087 1.5096 0.9608 22.6032
0.3 0.95394 1.266103673 0.3 1.96605 3.2933 37% 13.333 10 4.846561 0.90554 1.4537 0.9144 1.96605 1.4537 0.9144 33.2733
0.4 0.91652 1.159279481 0.4 2.16288 3.4278 25% 10 7.5 2.695407 0.82462 1.3745 0.8544 2.16288 1.3745 0.8544 43.1182
0.5 0.86603 1.047197551 0.5 2.4184 3.6276 16% 8 6 1.249387 0.70711 1.272 0.7862 2.4184 1.272 0.7862 51.8278
0.6 0.8 0.927295218 0.6 2.76787 3.927 9% 6.6667 5 0.354575 0.52915 1.1482 0.7157 2.76787 1.1482 0.7157 59.1877
0.7 0.71414 0.79539883 0.7 3.28533 4.3991 5% 5.7143 4.2857 0.001738 0.14142 1.01 0.6482 3.28533 1.01 0.6482 65.1567
0.8 0.6 0.643501109 0.8 4.16349 5.236 2% 5 3.75 0.354575 #NUM! 0.8709 0.5868 4.16349 0.8709 0.5868 69.8603
0.9 0.43589 0.451026812 0.9 6.17258 7.2073 0% 4.4444 3.3333 2.107014 #NUM! 0.7461 0.5327 6.17258 0.7461 0.5327 73.5139
0.999 0.14107 0.141539473 0.99 21.2668 22.27 0% 4.0404 3.0303 11.07817 #NUM! 0.6528 0.4902 21.2668 0.6528 0.4902 76.0935