NONLINEAR CONTROLLER COMPARISON ON A BENCHMARK ...
NONLINEAR CONTROLLER COMPARISON ON A BENCHMARK ... NONLINEAR CONTROLLER COMPARISON ON A BENCHMARK ...
Control Signal in Volts Response in cm 2 1.5 1 0.5 0 −0.5 −1 −1.5 −2 0 1 2 3 4 5 time 6 7 8 9 10 4 3 2 1 0 −1 −2 −3 Figure 4.1: Initial Open Loop Disturbance −4 0 1 2 3 4 5 time 6 7 8 9 10 Figure 4.2: Initial Open Loop Response 30
disturbances, whereas the hardware results will indicate the controls' performance in the presence of modeling errors, sensor noise, and other unmodelled disturbances. Plots showing how each of the six control laws compares to each of the others are included and discussed, but it is vital to have a more quantitative measure of performance. To this end a couple of simple methods were chosen to quantify the performance of the algorithms. First, a simple integrator was added that returns the total energy of the rst state (the beam's de ection) from t =2:5 to t = 10 seconds. This quanti es how quickly the oscillations died out which is the primary objective of the control laws. This sum also includes a measure of the steady state error of the controls, because most of the control laws achieved their steady states before t = 8 seconds. Second, an integrator returned the sum of the squared input signal from t = 2:5 to t = 10 seconds. This number represents the amount of energy used to implement the control: it provides an estimate of the control e ort, and it may thus be used to evaluate the e ciency of the control laws (i.e. if two control designs had comparable damping, which used less control e ort to achieve this damping?) These results are compared at the end of this section in tabular form. All of the simulations were conducted on the same SIMULINK model of the plant. Each of the control techniques was tuned extensively using the information from the simulations to yield the best possible performance. It should be noted that this process of tuning, of choosing the parameters in order to implement the controls at an optimal level, is a highly subjective activity. In fact there is no way to be sure that the parameters nally used yielded the best possible performance for the given implementation of the control strategy, though the utmost care was taken to try and achieve the best possible performance with each of the design strategies. 4.2 Evaluation of the Plots in Simulation 4.2.1 Linearized Optimal H 2 The standard linear quadratic regulation method successfully regulated the system, a fact which perhaps argues against this physical system as a benchmark for non-linear systems: the whole purpose of nonlinear control theory is to provide 31
- Page 1 and 2: NONLINEAR CONTROLLER COMPARISON ON
- Page 3 and 4: BRIGHAM YOUNG UNIVERSITY GRADUATE C
- Page 5 and 6: ABSTRACT NONLINEAR CONTROLLER COMPA
- Page 7 and 8: Contents Acknowledgments vi List of
- Page 9: List of Tables 4.1 Tabular Comparis
- Page 12 and 13: 4.19 SGA: Nonlinear H1 vs. Linear O
- Page 14 and 15: Figure 1.1: TORA System One of the
- Page 16 and 17: 1.3 Literature Review In surveying
- Page 19 and 20: Chapter 2 Plant Speci cations and M
- Page 21 and 22: Figure 2.2: Mechanical Model of Fle
- Page 23 and 24: Figure 2.4: Translational Oscillati
- Page 25 and 26: 2.3 Software Set-up All of the cont
- Page 27 and 28: Chapter 3 Overview of Control Strat
- Page 29 and 30: The optimal gain matrix was given b
- Page 31 and 32: 3.3 Passivity-Based Control Certain
- Page 33 and 34: limitations, k 1 and k 2 are tuning
- Page 35 and 36: Now we regard as the control variab
- Page 37 and 38: where V satis es the well known Ham
- Page 39 and 40: ecause one can quickly adjust the Q
- Page 41: Chapter 4 Simulation Results 4.1 Th
- Page 45 and 46: Response in cm 4 3 2 1 0 −1 −2
- Page 47 and 48: Response in cm Response in cm 4 3 2
- Page 49 and 50: Response in cm Response in cm 5 4 3
- Page 51 and 52: Response in cm 4 3 2 1 0 −1 −2
- Page 53 and 54: Response in cm Response in cm 4 3 2
- Page 55 and 56: Response in cm Response in cm 4 3 2
- Page 57 and 58: It is seen in Figure 4.23 that the
- Page 59: all of the physical parameters exce
- Page 62 and 63: Response in m 0.05 0.04 0.03 0.02 0
- Page 64 and 65: Response in m 0.05 0.04 0.03 0.02 0
- Page 66 and 67: Response in m Response in m 0.05 0.
- Page 68 and 69: Response in m Response in m 0.05 0.
- Page 70 and 71: Response in m Response in m 0.05 0.
- Page 72 and 73: control was that it requires only t
- Page 74 and 75: to the Galerkin approximation techn
- Page 77 and 78: Bibliography [1] P. Kokotovic M. Ja
disturbances, whereas the hardware results will indicate the controls' performance in<br />
the presence of modeling errors, sensor noise, and other unmodelled disturbances.<br />
Plots showing how each of the six control laws compares to each of the others<br />
are included and discussed, but it is vital to have a more quantitative measure of<br />
performance. To this end a couple of simple methods were chosen to quantify the<br />
performance of the algorithms. First, a simple integrator was added that returns the<br />
total energy of the rst state (the beam's de ection) from t =2:5 to t = 10 seconds.<br />
This quanti es how quickly the oscillations died out which is the primary objective<br />
of the control laws. This sum also includes a measure of the steady state error of the<br />
controls, because most of the control laws achieved their steady states before t = 8<br />
seconds. Second, an integrator returned the sum of the squared input signal from<br />
t = 2:5 to t = 10 seconds. This number represents the amount of energy used to<br />
implement the control: it provides an estimate of the control e ort, and it may thus<br />
be used to evaluate the e ciency of the control laws (i.e. if two control designs had<br />
comparable damping, which used less control e ort to achieve this damping?) These<br />
results are compared at the end of this section in tabular form.<br />
All of the simulations were conducted on the same SIMULINK model of the<br />
plant. Each of the control techniques was tuned extensively using the information<br />
from the simulations to yield the best possible performance. It should be noted that<br />
this process of tuning, of choosing the parameters in order to implement the controls<br />
at an optimal level, is a highly subjective activity. In fact there is no way to be sure<br />
that the parameters nally used yielded the best possible performance for the given<br />
implementation of the control strategy, though the utmost care was taken to try and<br />
achieve the best possible performance with each of the design strategies.<br />
4.2 Evaluation of the Plots in Simulation<br />
4.2.1 Linearized Optimal H 2<br />
The standard linear quadratic regulation method successfully regulated the<br />
system, a fact which perhaps argues against this physical system as a benchmark<br />
for non-linear systems: the whole purpose of nonlinear control theory is to provide<br />
31