REALISATION OF VARIABLE STRUCTURE SYSTEM FOR
ASTATIC AIRCRAFT CONTROL
Victor Glumov, Anatoly Syrov, Alexandr Puchkov
A solution of astatic attitude control problem for an aircraft is considered. The traditional solution method on the base of integral for the error can lead to the system dynamic accuracy breakdown. In the paper a contradiction between dynamic accuracy and the request of astatic control is solved on the base of variable structure control principle.