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The paper presents two new systems for identification and neuro-adaptive command with direct applicability to the control of the longitudinal and lateral aircrafts movement and to the rockets vertical and horizontal movement. Also, one presents a structure for the parametric estimation and discrete optimal command of the aircrafts movement. The design of these structures is based on the algorithms that belong to the authors of this paper. Theoretical results are validated by numerical simulations; the authors obtained Matlab/Simulink models and calculus programs for the identification, neuro-adaptive command, on-line estimation and discrete command of the aircrafts movement, respectively.

New Systems for Identification, Estimation and Adaptive Control of the Aircrafts Movement