combinepdf
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
INTEGRATION OF SC METHODOLOGIES<br />
WITH SLIDING MODE CONTROL<br />
RING<br />
Ms. RINU ALICE KOSHY,<br />
ASST.PROFESSOR, DEE<br />
Fundamentals of SMC<br />
The SMC theory was originated in late 1950s in the former USSR, led by Prof.<br />
V. I. Utkin and Prof. S. V. Emelyanov [2] to address specific problems associated<br />
with a special class of VSSs, which are the control systems involving<br />
discontinuous control actions.<br />
In the early days of VSS, the research was focused on single-input and singleoutput<br />
systems, and various well-known methodologies were developed, e.g., the<br />
eigen value assignment approach [2], the Fillipov approach [5], etc. In recent<br />
years, the majority of research in SMC has been done with regard to multiinput<br />
and multioutput systems (MIMO), so we will use MIMO system framework as a<br />
platform for discussing the integration of SC methodologies in SMC. Commonly,<br />
the MIMO SMC systems considered are of the form<br />
ẋ˙ = f(x, t) + B(x, t)u + ξ(x, t)<br />
where<br />
x ∈ R n u is the system state vector and ξ(x, t) ∈ Rn represents all the factors<br />
that affect the performance of the control system, such as disturbances and<br />
uncertainties in the parameters of the system.<br />
.It is well known that when this condition (the matching condition) is satisfied,<br />
the celebrated invariance property of SMC stands.<br />
The design procedure of SMC includes two major steps encompassing two main<br />
phases of SMC:<br />
1) Reaching phase: where the system state is driven from any initial state to<br />
reach the switching manifolds (the anticipated sliding modes) in finite time;<br />
2) Sliding-mode phase: where the system is induced into the sliding motion on<br />
the switching manifolds, i.e., the switching manifolds become an attractor. These<br />
two phases correspond to the following two main design steps.<br />
1) Switching manifold selection: A set of switching manifolds are selected with<br />
prescribed desirable dynamical characteristics. Common candidates are linear<br />
hyper-planes.<br />
2) Discontinuous control design: A discontinuous control strategy is formed to<br />
ensure the finite time reachability of the switching manifolds. The controller may<br />
be either local or global, depending upon specific control requirements.<br />
In the context of the system (1), following the main SMC design steps, the<br />
switching manifolds can be denoted as<br />
s(x) = 0 ∈ Rm, where s = (s1, . . . , sm)T