Abstract
—The Sliding and Integral Sliding Mode
control design anticipated to handle out the crosscoupling effects in a twin rotor system. These crosscoupling effects lead to tainted act during precise
maneuvering of twin rotor system. These cross-coupling
effects can be concealed by introducing decoupling
procedures such as Sliding and Integral Sliding Mode
Controls. These controllers propose sturdiness at the
rate of achievement to triumph over the cross-coupling
in order to achieve the desired performance. The
performances of both controllers are compared. This
initiative has been effectively proved by simulations.
Muhammad Taimoor, Sohail Iqbal, Abdul Waheed. (2015) Sliding and Integral Sliding Mode Control Design for Twin Rotor System, Journal of Space Technology , Volume 5, Issue 1.
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