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Grinding mill circuit control from a plant-wide control perspectiveLe Roux, Johan Derik January 2016 (has links)
A generic plant-wide control structure is proposed for the optimal operation of a grinding mill circuit.
An economic objective function is defined for the grinding mill circuit with reference to the economic
objective of the larger mineral processing plant. A mineral processing plant in this study consists of a
comminution and a separation circuit and excludes the extractive metallurgy at a metal refinery. The
comminution circuit's operational performance primarily depends on the mill's performance. Since
grindcurves define the operational performance range of a mill, the grindcurves are used to define
the setpoints for the economic controlled variables for optimal steady-state operation. For a given
metal price, processing cost, and transportation cost, the proposed structure can be used to define
the optimal operating region of a grinding mill circuit for the best economic return of the mineral
processing plant. The plant-wide control structure identifies the controlled and manipulated variables
to ensure the grinding mill circuit can be maintained at the desired operating condition.
The plant-wide control framework specifies regulatory and supervisory control aims which can be
achieved by means of non-linear model-based control. An impediment to implementing model-based
control is the computational expense to solve the non-linear optimisation function. To resolve this
issue, the reference-command tracking version of model predictive static programming (MPSP) is
applied to a grinding mill circuit. MPSP is an innovative optimal control technique that combines
the philosophies of Model Predictive Control (MPC) and approximate dynamic programming. The
performance of the proposed MPSP control technique, is compared to the performance of a standard
non-linear MPC (NMPC) technique applied to the same plant for the same conditions. Results show
that the MPSP control technique is more than capable of tracking the desired set-point in the presence
of model-plant mismatch, disturbances and measurement noise. The performance of MPSP and NMPC
compare very well, with definite advantages offered by MPSP. The computational speed of MPSP
is increased through a sequence of innovations such as the conversion of the dynamic optimization
problem to a low-dimensional static optimization problem, the recursive computation of sensitivity
matrices, and using a closed form expression to update the control. The MPSP technique generally
takes only a couple of iterations to converge, even when input constraints are applied. Therefore,
MPSP can be regarded as a potential candidate for on-line applications of the NMPC philosophy to
real-world industrial process plants.
The MPSP and NMPC simulation studies above assume full-state feedback. However, this is not always
possible for industrial grinding mill circuits. Therefore, a non-linear observer model of a grinding mill
is developed which distinguishes between the volumetric hold-up of water, solids, and the grinding
media in the mill. Solids refer to all ore small enough to discharge through the end-discharge grate,
and grinding media refers to the rocks and steel balls. The rocks are all ore too large to discharge from
the mill. The observer model uses the accumulation rate of solids and the discharge rate as parameters.
It is shown that with mill discharge flow-rate, discharge density, and volumetric hold-up measurements,
the model states and parameters are linearly observable. Although instrumentation at the mill discharge
is not yet included in industrial circuits because of space restrictions, this study motivates the benefits
to be gained from including such instrumentation. An Extended Kalman Filter (EKF) is applied
in simulation to estimate the model states and parameters from data generated by a grinding mill
simulation model from literature. Results indicate that if sufficiently accurate measurements are
available, especially at the discharge of the mill, it is possible to reliably estimate grinding media,
solids and water hold-ups within the mill. Such an observer can be used as part of an advanced process
control strategy. / 'n Generiese aanlegwye beheerstruktuur vir die optimale beheer van 'n maalmeulkring word voorgehou.
'n Ekonomiese doelwitfunksie is gedefinieer vir die maalmeulkringbaan met verwysing tot die
ekonomiese doelwit van die groter mineraalverwerkingsaanleg. 'n Mineraalverwerkingsaanleg bestaan
in hierdie studie slegs uit die vergruisings- en skeidingskringbane. Die ekstraktiewe metallurgie by
die metaal raffinadery word uitgesluit. Die vergruisingskringbaan se operasionele werksverrigting is
hoofsaaklik van die maalmeul se werksverrigting afhanklik. Aangesien maalkurwes die bereik van
die maalmeul se werksverrigting beskryf, kan die maalkurwes gebruik word om die stelpunte van die
ekonomiese beheerveranderlikes te definieer vir werking by optimale gestadigde toestand. Gegewe
'n bepaalde metaalprys, bedryfskoste, en vervoerkoste, kan die voorgestelde struktuur gebruik word
om die optimale werksgebied vir die maalmeulkring te definieer vir die beste ekonomiese gewin van
die algehele mineraalverwerkingsaanleg. Die aanlegwye beheerstruktuur omskryf die beheerveranderlikes
en manipuleerbare veranderlikes wat benodig word om die maalmeulkring by die gewenste
werksgebied te handhaaf. Die aanlegwye beheerstruktuur spesifiseer regulatoriese en toesighoudende beheer doelwitte. Hierdie
doelwitte kan bereik word deur gebruik te maak van nie-lineêre model gebaseerde beheer. Die probleem
is dat die bewerkingskoste om nie-lineëre optimeringsfunksies op te los 'n struikelblok is om model
gebaseerde beheer op industriële aanlegte toe te pas. Ter oplossing hiervan, word die stelpunt-volg
weergawe van model gebaseerde voorspellende statiese programmering (MVSP) toegepas op 'n
maalmeulkringbaan. MVSP is 'n innoverende optimale beheertegniek, en bestaan uit 'n kombinasie
van die filosofieë van model gebaseerder voorspellende beheer (MVB) en aanpassende dinamiese
programmering. Die verrigting van die voorgestelde MVSP beheertegniek word vergelyk met die
verrigting van 'n standaard nie-lineëre MVB (NMVB) tegniek deur beide beheertegnieke op dieselfde
aanleg vir dieselfde toestande toe te pas. Resultate dui aan dat die MVSP beheertegniek in staat is
om die gekose stelpunt te midde van model-aanleg wanaanpassing, steurnisse, en metingsgeraas te
volg. Die verrigting van MVSP en NMVB vergelyk goed, maar MVSP bied duidelike voordele. Die
bewerkingspoed vir MVSP word vinniger gemaak deur die dinamiese optimeringsprobleem in 'n laeorde
statiese optimeringsprobleem te omskep, die sensitiwiteitsmatrikse rekursief uit te werk, en deur
'n geslote uitdrukking ter opdatering van die beheeraksie te gebruik. Die MVSP beheertegniek benodig
normaalweg slegs 'n paar iterasies om tot 'n oplossing te konvergeer, selfs indien beperkings op die
insette toegepas word. Om die rede word MVSP as 'n potensiële kandidaat beskou vir aanlyntoepasings
van die NMVB filosofie op industriële aanlegte.
Die MVSP en NMVB simulasie studies hierbo neem aan dat volle toestandterugvoer moontlik is.
Hierdie is nie altyd moontlik vir industriële maalmeulkringbane nie. Om die rede is 'n nie-lineêre
waarnemingsmodel van 'n maalmeul ontwikkel. Die model onderskei tussen die volumetriese hoeveelheid
water, vaste stowwe, en maalmedia in die meul. Vaste stowwe verwys na alle erts wat klein
genoeg is om deur die uitskeidingsif aan die ontslagpunt van die meul te vloei. Maalmedia verwys
na rotse en staalballe in die meul, met rotse wat te groot is om deur die uitskeidingsif te vloei. Die
waarnemingsmodel maak gebruik van die ontslaantempo en die opeenhopingstempo van vaste stowwe
as parameters. Indien die meul se ontslagvloeitempo, ontslagdigtheid, en totale volumetriese aanhouding
gemeet word, is alle toestande en parameters van die waarnemingsmodel lineêr waarneembaar.
Alhoewel instrumentasie by die meul se ontslagpunt as gevolg van ruimte beperkings nog nie op
industriële aanlegte ingesluit word nie, dui hierdie studie die voordele aan wat verkrygbaar is deur
sulke instrumentasie in te sluit. 'n Verlengde Kalman Filter (VKF) word in simulasie gebruik om
die model se toestande en parameters af te skat. 'n Bestaande maalmeul simulasie model vanuit die
literatuur word gebruik om die nodige data vir die VKF te genereer. Resultate dui aan dat indien die metings akkuraat genoeg is, veral by die ontslagpunt van die meul, betroubare afskattings van die
volumetriese hoeveelheid maalmedia, vaste stowwe, en water in die meul gemaak kan word. So 'n
afskatter kan vorentoe gebruik word as deel van 'n gevorderde prosesbeheer strategie. / Thesis (PhD)--University of Pretoria, 2016. / Electrical, Electronic and Computer Engineering / PhD / Unrestricted
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Advanced Optimal Control Design for Nonlinear Systems including Impulsive Inputs with Applications to Automatic Cancer TreatmentSakode, Chandrashekar M January 2015 (has links) (PDF)
The motivation of this research is to propose innovative nonlinear and optimal control design algorithms, which can be used in real life. The algorithms need to be computationally efficient, should deal with control constraints and should operate under state feedback. To show the efficacy of algorithms, automatic therapy for different cancer problems is chosen to be the field of application.
In this thesis, first an advanced control design technique called ’optimal dynamic in-version’ has been successfully experimented with control constraints. The proposed approach has subsequently been shown to be quite effective in proposing automatic drug delivery schemes with simultaneous application of chemo and immunotherapy drugs for complete elimination of cancer cells in melanoma (a skin cancer) as well as glioma (a brain cancer). As per the current practice, the amount of drug dosages are generally given based on some apriori statistical study with a very small sample size, which in reality may either also lead to drug toxicity (due to excessive drug) or may become ineffective (due to insufficient drug) for a particular patient. Subject to the fidelity of the mathematical model (which has been taken from published literature), it has been shown in this thesis that nonlinear control theory can be used for computation of drug dosages, which can then be used in a feedback strategy, thereby customizing the drug for the patient’s condition, to cure the disease successfully.
Next, attention has been shifted to impulsive control of systems. Such impulsive con-trol systems appear in many other applications such as control of swings, control of spacecrafts and rockets using reaction control system, radiotherapy in cancer treatment and so on. Two impulsive control design philosophies are proposed in this thesis. In one approach, recently proposed model predictive static programming (MPSP) has been extended for impulsive control systems and has been named as impulsive-MPSP (I-MPSP). In other approach, another recent development, namely the Pseudospectral method has been utilized to consider both the magnitude of the control impulses as well as the time instants at which they are applied as the decision variables. It can be noted, that to the best of the knowledge of the author, the time instants of control application, being considered as decision variables is being proposed for the first time in the nonlinear and optimal control framework. Both I-MPSP and Pseudospectral methods are computationally quite efficient and hence can be used for feedback control (I-MPSP happens to be computationally more efficient than the Pseudospectral method). Applicability of the proposed extensions have been shown by solving various benchmark problems such as (i) a scalar linear problem, (ii) Van der Pol’s oscillator problem and (iii) an inverted pendulum problem. Finally the applicability of the proposed I-MPSP strategy has been shown by solving challenging problems such as radiotherapy treatment of head and neck and adenocarcimona cancers. Radio-therapy model is considered with oxygen effect, in which radiosensitivity parameters are considered in different forms. Head and neck cancer is considered with constant radiosensitivity parameters and adenocarcinoma is considered with constant, linear, quadratic and saturation model of radiosensitivity parameters. Note that toxicity constraints on normal tissue, which are nonlinear control constraints, are also successfully incorporated in this control design.
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Optimal Guidance Of Aerospace Vehicles Using Generalized MPSP With Advanced Control Of Supersonic Air-Breathing EnginesMaity, Arnab 12 1900 (has links) (PDF)
A new suboptimal guidance law design approach for aerospace vehicles is proposed in this thesis, followed by an advanced control design for supersonic air-breathing engines. The guidance law is designed using the newly developed Generalized Model Predictive Static Programming (G-MPSP), which is based on the continuous time nonlinear optimal control framework. The key feature of this technique is one-time backward propagation of a small-dimensional weighting matrix dynamics, which is used to update the entire control history. This key feature, as well as the fact that it leads to a static optimization problem, lead to its computational efficiency. It has also been shown that the existing model predictive static programming (MPSP), which is based on the discrete time framework, is a special case of G-MPSP. The G-MPSP technique is further extended to incorporate ‘input inequality constraints’ in a limited sense using the penalty function philosophy. Next, this technique has been developed also further in a ‘flexible final time’ framework to converge rapidly to meet very stringent final conditions with limited number of iterations.
Using the G-MPSP technique in a flexible final time and input inequality constrained formulation, a suboptimal guidance law for a solid motor propelled carrier launch vehicle is successfully designed for a hypersonic mission. This guidance law assures very stringent final conditions at the injection point at the end of the guidance phase for successful beginning of the hypersonic vehicle operation. It also ensures that the angle of attack and structural load bounds are not violated throughout the trajectory. A second-order autopilot has been incorporated in the simulation studies to mimic the effect of the inner-loops on the guidance performance. Simulation studies with perturbations in the thrust-time behaviour, drag coefficient and mass demonstrate that the proposed guidance can meet the stringent requirements of the hypersonic mission.
The G-MPSP technique in a fixed final time and input inequality constrained formulation has also been used for optimal guidance of an aerospace vehicle propelled by supersonic air-breathing engine, where the resulting thrust can be manipulated by managing the fuel flow and nozzle area (which is not possible in solid motors). However, operation of supersonic air-breathing engines is quite complex as the thrust produced by the engine is a result of very complex nonlinear combustion dynamics inside the engine. Hence, to generate the desired thrust, accounting for a fairly detailed engine model, a dynamic inversion based nonlinear state feedback control design has been carried out. The objective of this controller is to ensure that the engine dynamically produces the thrust that tracks the commanded value of thrust generated from the guidance loop as closely as possible by regulating the fuel flow rate. Simultaneously, by manipulating throat area of the nozzle, it also manages the shock wave location in the intake for maximum pressure recovery with sufficient margin for robustness. To filter out the sensor and process noises and to estimate the states for making the control design operate based on output feedback, an extended Kalman filter (EKF) based state estimation design has also been carried out and the controller has been made to operate based on estimated states. Moreover, independent control designs have also been carried out for the actuators so that their response can be faster. In addition, this control design becomes more challenging to satisfy the imposed practical constraints like fuel-air ratio and peak combustion temperature limits. Simulation results clearly indicate that the proposed design is quite successful in assuring the desired performance of the air-breathing engine throughout the flight trajectory, i.e., both during the climb and cruise phases, while assuring adequate pressure margin for shock wave management.
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