A Statistical Analysis of Commercial Aviation Accidents, Technical Report, vol.Airbus, 1958. ,
Design of the flare control law for longitudinal autopilot using H/sub infinity / synthesis, 29th IEEE Conference on Decision and Control, pp.5-7, 1990. ,
DOI : 10.1109/CDC.1990.203331
A New Approach to Fixed-order H ? Synthesis: Application to Autoland Design, Proceedings of the AIAA Guidance, Navigation, and Control Conference, pp.6-9, 2001. ,
Design of Autoland Controller Functions with Multiobjective Optimization, Journal of Guidance, Control, and Dynamics, vol.3, issue.2, pp.475-484, 2006. ,
DOI : 10.1080/00207179408923070
Final Approach and Flare Control of a Flexible Aircraft in Crosswind Landings, Journal of Guidance, Control, and Dynamics, vol.18, issue.1, pp.946-957, 2013. ,
DOI : 10.1017/CBO9780511809170
Robust nonlinear motion control of a helicopter, IEEE Transactions on Automatic Control, vol.48, issue.3, pp.413-426, 2003. ,
DOI : 10.1109/TAC.2003.809147
Design and implementation of an autonomous flight control law for a UAV helicopter, Automatica, vol.45, issue.10, pp.2333-2338, 2009. ,
DOI : 10.1016/j.automatica.2009.06.016
Multimodel eigenstructure assignment in flight-control design, Aerospace Science and Technology, vol.3, issue.3, pp.141-151, 1999. ,
DOI : 10.1016/S1270-9638(99)80038-8
H-Infinity Robust Control Design for the NASA AirSTAR Flight Test Vehicle, 50th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, pp.9-12, 2012. ,
DOI : 10.2514/6.2012-1181
Nonsmooth<tex>$H_infty$</tex>Synthesis, IEEE Transactions on Automatic Control, vol.51, issue.1, pp.71-86, 2006. ,
DOI : 10.1109/TAC.2005.860290
Stabilization via Nonsmooth, Nonconvex Optimization, IEEE Transactions on Automatic Control, vol.51, issue.11, pp.1760-1769, 2006. ,
DOI : 10.1109/TAC.2006.884944
URL : http://homepages.laas.fr/henrion/Papers/chocolate.pdf
Multi-model, multi-objective tuning of fixed-structure controllers, 2014 European Control Conference (ECC), pp.24-27, 2014. ,
DOI : 10.1109/ECC.2014.6862200
Flare Control Law Design via Multi-Channel H ? Synthesis: Illustration on a Freely Available Nonlinear Aircraft Benchmark, Proceedings of the American Control Conference, pp.17-19, 2015. ,
Essential of Robust Control, 1998. ,
Nonlinear Structured H ? Controllers for Parameter-Dependent Uncertain Systems with Application to Aircraft Landing, pp.13-15 ,
URL : https://hal.archives-ouvertes.fr/hal-01653172
A Civilian Aircraft Landing Challenge. Online Available from the Aerospace Benchmark Section of the SMAC Toolbox, Available, vol.online ,
Robust Flare Control Design Using Structured H ??? Synthesis: a Civilian Aircraft Landing Challenge, Proceedings of the 20th IFAC World Congress, pp.9-14, 2017. ,
DOI : 10.1016/j.ifacol.2017.08.769
URL : https://research-information.bristol.ac.uk/files/145142662/IFAC_2017_DiegoNavarro_v4_FinalSubmission.pdf
Robust Autopilot Design for Crosswind Landing This article is an open access article distributed under the terms and conditions of the Creative Commons Attribution (CC BY) license (http, Proceedings of the 20th IFAC World Congress, pp.9-14, 2017. ,