NONLINEAR CONTROLLER COMPARISON ON A BENCHMARK ...
NONLINEAR CONTROLLER COMPARISON ON A BENCHMARK ...
NONLINEAR CONTROLLER COMPARISON ON A BENCHMARK ...
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1.3 Literature Review<br />
In surveying the technical literature relevant to this thesis, there are two pri-<br />
mary topics: research on the topic of the successive Galerkin approximation method,<br />
and research devoted to the topic of the NLBP system. Additionally a short review of<br />
the literature pertaining to the various control strategies used to highlight the SGA<br />
method will be presented.<br />
The SGA method was rst published in [3] as a method for iteratively improv-<br />
ing a nonlinear feedback control. This publication included a proof of the algorithm's<br />
convergence and the stability of the resulting control law at each iteration. Addi-<br />
tionally, each iteration brings the control design closer to solving the HJB equation,<br />
and thus the method of successive approximation eventually yields an approxima-<br />
tion of the nonlinear optimal solution with any desired accuracy, as the order of the<br />
Galerkin approximation increases and as the number of iterations goes to in nity.<br />
In [4] the algorithm was successfully applied to the inverted pendulum problem as<br />
well as several one-dimensional examples. In [5] the SGA technique was extended to<br />
the optimal robust nonlinear control problem. In the robust problem, a solution of the<br />
Hamilton-Jacobi-Isaacs equation is required with the minimum possible L 2 gain from<br />
disturbance to output. In [5] a proof is presented of the convergence and stability of<br />
the algorithm at each successive iteration, and su cient conditions for convergence<br />
and stability are presented for both the nonlinear optimal and robust algorithms.<br />
Additionally, [5] successfully applies the algorithm to a hydraulic actuation system,<br />
a missile autopilot design, and the control of an underwater vehicle system.<br />
The control of the TORA system was originally proposed as a model of a<br />
dual-spin spacecraft. The goal was to study how to circumvent the resonance capture<br />
e ect in [6], but in [7], [8] the system was studied to analyze the usefulness of a<br />
rotational actuator in damping out linear oscillations and vibrations. It was rst<br />
proposed as a benchmark problem for nonlinear control systems in [2]. A physical<br />
testbed is described consisting of a motor driven proof mass that was mounted on a<br />
linear air track. In [2], the three-fold objective of the Nonlinear Benchmark Problem<br />
is set forth: to stabilize the closed loop system, to exhibit good disturbance rejection<br />
4