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Model Predictive Flight Control System with Full State Observer using H∞ Method
Abstract This paper presents the application of the model predictive approach to design a flight control system (FCS) for longitudinal dynamics of a fixed wing aircraft. Longitudinal dynamics is derived for a conventional aircraft. Open loop aircraft response analysis is carried out. Simulation studies are illustrated to prove the efficacy of the proposed model predictive controller using H ∞ state observer. The estimation criterion used in the observer design is to minimize the worst possible effects of the modelling errors and additive noise on the parameter estimation.
Model Predictive Flight Control System with Full State Observer using H∞ Method
Abstract This paper presents the application of the model predictive approach to design a flight control system (FCS) for longitudinal dynamics of a fixed wing aircraft. Longitudinal dynamics is derived for a conventional aircraft. Open loop aircraft response analysis is carried out. Simulation studies are illustrated to prove the efficacy of the proposed model predictive controller using H ∞ state observer. The estimation criterion used in the observer design is to minimize the worst possible effects of the modelling errors and additive noise on the parameter estimation.
Model Predictive Flight Control System with Full State Observer using H∞ Method
Sanwale, Jitu (Autor:in) / Singh, Dhan Jeet (Autor:in)
Journal of The Institution of Engineers (India): Series C ; 100 ; 323-332
02.03.2018
10 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
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