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Assessment and Future Directions of Nonlinear Model Predictive ...

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224 C.E. Long <strong>and</strong> E.P. GatzkeVd3CV2V34V44TANK 3TANK 4High PressureAir FeedP3V32P4P1V14P2V22TANK 1TANK 2CV1V12Vd1Fig. 1. Schematic <strong>of</strong> the Network <strong>of</strong> Pressure TanksSupply air is fed to the system at 60 psig through two control valves whichact as the manipulated variables (u 1 <strong>and</strong> u 2 ) in the control problem. Pressuregradients drive the flow <strong>of</strong> air through the system. The air flows through thefour tanks that are interconnected, while the numerous valves throughout thesystem dictate the direction <strong>of</strong> the flow. After traveling through the system,the air ultimately exits the downstream tanks to the atmosphere. It is assumedthat the pressure in each <strong>of</strong> the four tanks can be measured. These will act asthe process outputs to be controlled. The non-square nature <strong>of</strong> this configuration(2×4) lends itself well to demonstrating the ability <strong>of</strong> this specific controller as allfour measurements cannot be maintained at setpoint using only two manipulatedvariables, thus forcing the controller to decide the appropriate trade-<strong>of</strong>f basedon the prioritized objectives.For this work, it is assumed that the flow <strong>of</strong> air across a given valve (v i )canbe defined as:√f i (k) =c i ∆Pi (k) (4)where f i is a molar flow, k is the sample time, c i is a proportionality constantrelated to the valve coefficient, <strong>and</strong> ∆P i is the pressure drop across the valve.For this study, it is assumed that there is no reverse flow across a valve, forcing∆P i non-negative. Under ideal conditions, the discrete time governing equationsdefining the pressures in each tank are taken as:P 1 (k +1)= hP1(k)V 1(u 1 f CV 1 − γ 1 f 12 − (1 − γ 1 )f 14 )+P 1 (k)P 2 (k +1)=hP2(k)V 2(γ 1 f 12 +(1− γ 2 )f 32 − f 22 )+P 2 (k)P 3 (k +1)= hP3(k)V 3(u 2 f CV 2 − γ 2 f 34 − (1 − γ 2 )f 32 )+P 3 (k)P 4 (k +1)= (γ 2 f 34 +(1− γ 1 )f 14 − f 44 )+P 4 (k)hP4(k)V 4where γ 1 <strong>and</strong> γ 2 define the fractional split <strong>of</strong> air leaving the upstream tanks.Here, this set <strong>of</strong> equations represents both the nonlinear process <strong>and</strong> the modelused for control purposes. The sampling period (h) used was 3 minutes. This isimportant as it defines the time limit in which each optimization problem mustbe solved for real-time operation. The parameter values used in this study aresummarized in Table 1.(5)

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