This paper proposes an alternative formulation of the guidance problem, particularly suitable in autonomous aircraft applications. The Lyapunov’s direct method is adopted as main tool to prove some properties of the considered guidance law. The aim of this work is designing a new feedback implemented algorithm that asymptotically stabilizes a generic aircraft to the imposed reference bearing in a local earth reference frame, instead of the velocity vector stabilization towards a reference way–point.
AIRCRAFT GUIDANCE LAW ANALYSIS / W.GERI; BERTONI G.. - STAMPA. - (2004). (Intervento presentato al convegno 16th IFAC Symposium on Automatic Control in Aerospace -San Pietroburgo (Russia) nel 13-18 Giugno 2004).
AIRCRAFT GUIDANCE LAW ANALYSIS
GERI, WALTER;BERTONI, GIANNI
2004
Abstract
This paper proposes an alternative formulation of the guidance problem, particularly suitable in autonomous aircraft applications. The Lyapunov’s direct method is adopted as main tool to prove some properties of the considered guidance law. The aim of this work is designing a new feedback implemented algorithm that asymptotically stabilizes a generic aircraft to the imposed reference bearing in a local earth reference frame, instead of the velocity vector stabilization towards a reference way–point.I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
