| Issue |
Volume 6, 2013
Progress in Flight Dynamics, Guidance, Navigation, Control, Fault Detection, and Avionics
|
|
|---|---|---|
| Page(s) | 729 - 748 | |
| Section | Flexible aircraft control | |
| DOI | https://doi.org/10.1051/eucass/201306729 | |
| Published online | 02 December 2013 | |
A linear parameter-varying multiobjective control law design based on youla parametrization for a flexible blended wing body aircraft
ONERA 2 Avenue Edouard Belin BP74025 Toulouse 31055, France
This article presents a methodology for a linear parameter-varying (LPV) multiobjective flight control law design for a blended wing body (BWB) aircraft and results. So, the method is a direct design of a parametrized control law (with respect to some measured flight parameters) through a multimodel convex design to optimize a set of specifications on the full-flight domain and different mass cases. The methodology is based on the Youla parameterization which is very useful since closed loop specifications are affine with respect to Youla parameter. The LPV multiobjective design method is detailed and applied to the BWB flexible aircraft example.
© Owned by the authors, published by EDP Sciences, 2013
This is an Open Access article distributed under the terms of the Creative Commons Attribution License 2.0, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.