Power system control law reconfiguration on basis of systems embedding approach

Abstract

A control system reconfiguration problem for various failures is presented. The derived reconfiguration algorithm allows not only compensating the failure effects but remaining the dynamic performances of object in free and forced movements constant.

Aircraft Control Law Reconfiguration

“…The algorithm is based on an analytical procedure for the synthesis of multivariable system control laws developed by authors of (Glasov, Kosjanchuk 2010;Kosjanchuk, Zybin 2002;Kosjanchuk 2002;Misrikhanov et al 2005). The essence of the algorithm is an analytical solution of a matrix equation (Bukov et al 2002) connecting flight parameters, effectiveness of controls before and after the failure, and the special coefficients for control action redistribution to the operable control surfaces.…”