Optimal Control of Flying Objects ’ Move After Estimated State Vector Using a Reduced Order Observer

Abstract:- In this paper one presents an algorithm for project of a reduced order observer (ALGLOOR) with applications to flying objects ’ move. The command law is an optimal one in rapport with state vector of the observer. Numeric calculus examples are also presented: for longitudinal and lateral move and vertical move of a rocket in vertical plane in rapport with equal signal line; using Matlab/Simulink model of closed loop system one has made numeric calculus programs and with them one obtained different time characteristics, which expresses state variables ’ dynamics of the flying objects dynamic models