Abstract: For modern airplanes, it is usually needed to install more control effectors to realize the application of advanced technique and to satisfy the requirements of reliability and maneuverability. For optimal purpose of the efficiencies of the installed effectors in combination, it is needed to deploy the factors such as the installation location and installation angle. In this paper, by using Moore-Penrose inversion method borrowed from aircraft reconfigurable control method, a set of direct control redundance methods is brought up and the optimal control efficiencies of different effector deployments core obtained. The feasibility of the method proposed is verified by the aerodynamic data of a certain type of native airplane with V-shape vertical tail in flight balance state.

Key words: effectors deployment, control efficiency, Moore-Penrose inverse, direct control redundance, V-shape vertical tail