This article presents the development of fly-by-wire control laws used for the highfidelity simulation of a new transport category aircraft. Beyond structural and gain design aspects for normal operations, envelope protections and limitations as well as mode transition issues are also addressed. As the control system is to be adjusted to changing aircraft datasets at different levels of fidelity, particular emphasis has been put on a high level of automation in gain design and system assessment routines. For lateral dynamics, eigenstructure assignment is used as the design methodology whereas pole placement is used for the pitch axis.
Development of control laws for the simulation of a new transport aircraft
Entwicklung von Regelungsgesetzen zur Simulation neuer Transportflugzeuge
2009
16 Seiten, 9 Bilder, 8 Quellen
Article (Journal)
English
Development of control laws for the simulation of a new transport aircraft
SAGE Publications | 2009
|Development of control laws for the simulation of a new transport aircraft
Online Contents | 2009
|Aircraft Control Laws for Envelope Protection
AIAA | 2006
|