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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