Analytical synthesis of longitudinal motion control laws for single-rotor helicopter
The control laws analytical expressions are receive for the linearized model of longitudinal motion of single-rotor helicopter fourth-order. The original decomposition of the object control and modal control method according to MIMO system state which is previously developed by the authors on its basis is assumed as basis of synthesis. The method does not require special solutions of matrix equations (equations like Sylvester), has the same kind for continuous and discrete cases of the model system setting, has no restrictions on algebraic and geometric multiplicity given by the poles, is easy implemented in MATLAB medium. The results control numerical modeling results of the single-rotor helicopter longitudinal movement by using the analytically synthesized control laws, which represent graphs of transients processes and control actions are adduced.