OPTIMAL OBSERVER-BASED CONTROL DESIGN FOR AIRCRAFT LATERAL MOTION

The paper presents an alternative approach of observer-based flight control system design. This approach is based on the application of linear matrix inequality technique. The design procedure treats the design of both observer and controller by solving the set of linear inequalities simultaneously. The proposed approach is free of observer poles placement location. Simulation results demonstrate the validity and effectiveness of the proposed design approac

Intelligent Flight Control System Design for the Small UAV Based on the Adaptive Neuro-Fuzzy Inference System

The paper considers a problem of flight control system design for small unmanned aerial vehicle with elements of intelligent control. The design procedure is illustrated by an example of unmanned aerial vehicle longitudinal control with application of adaptive neurofuzzy inference model.Рассмотрена задача синтеза системы управления полетом малого беспилотного летательного аппарата с элементами искусственного интеллекта. Процедура синтеза показана на примере управления продольным движением беспилотного летательного аппарата с использованием адаптивной нейро-нечеткой модели.Розглянуто задачу синтезу системи керування польотом малого безпілотного літального апарату з елементами штучного інтелекту. Процедуру синтезу показано на прикладі керування повздовжнім рухом безпілотного літального апарату з використанням адаптивної нейро-нечіткої моделі

OPTIMAL OBSERVER-BASED CONTROL DESIGN FOR AIRCRAFT LATERAL MOTION

The paper presents an alternative approach of observer-based flight control system design. This approach is based on the application of linear matrix inequality technique. The design procedure treats the design of both observer and controller by solving the set of linear inequalities simultaneously. The proposed approach is free of observer poles placement location. Simulation results demonstrate the validity and effectiveness of the proposed design approac