Flight Control System Design based on the Eigenstructure Assignment

초록

The flight control system of an aircraft functions to supplement its safety and efficeint operation, such that the desired flight mission can be accomplished and unexpected situation can be managed. The flight control system for pre-presented aircraft is designed by the theory of the eigenstructure assignement. The fligjt control system is designed by classical approach which consists of splitting up the controller into two parts, a longitudinal and a lateral controller. Also they have the standard inner-outer loop control structure. In spite of the controller simplicity, good performance results are obtained through the linear simulations.