Numerical Approach to Inverse Flight Dynamics

We develop a general numerical approach to inverse problems of vehicle dynamics, suitable for both fixed- and rotating-wing aircrafts. The formulation is based on an energy-preserving finite element in time for rigid body dynamics that ensures unconditional stability according to the energy method....

Ausführliche Beschreibung

Bibliographische Detailangaben

Veröffentlicht in:	Journal of guidance, control, and dynamics control, and dynamics, 1997-07, Vol.20 (4), p.742-747
Hauptverfasser:	Borri, Marco, Bottasso, Carlo L, Montelaghi, Fabio
Format:	Artikel
Sprache:	eng
Schlagworte:	Aerodynamics Aircraft Boundary conditions Finite element method Inverse problems Kinematics Problem solving
Online-Zugang:	Volltext
Tags:	Tag hinzufügen Keine Tags, Fügen Sie den ersten Tag hinzu!