Robustness stability and robust performance of the automatic flight control systems
Date : 2002
Journal title : AARMS
Journal volume : 1
Journal issue number : 2
Pages : 253-269
Document type : Folyóiratcikk
Subject : repülés, irányítás, repülésbiztosítás, repülőgép-elektronika, repülőgép-irányítás, katonai műszaki tudományok
Abstract :
This paper deals with the analysis of the robustness stability and robust performance of
the pitch rate stability augmentation system. Dynamics of the fuselage elastic bending
motion will be considered for additive uncertainty. The purpose of the authors is to
analyze if the given controller is able to stabilize the aircraft motion when its true
dynamics is taken into account during controller gain selection.
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