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andres marcos
andres marcos
Universidad Carlos III de Madrid & Technology for Aerospace Control Ltd.
Bestätigte E-Mail-Adresse bei ing.uc3m.es - Startseite
Titel
Zitiert von
Zitiert von
Jahr
Development of linear-parameter-varying models for aircraft
A Marcos, GJ Balas
Journal of Guidance, Control, and Dynamics 27 (2), 218-228, 2004
4572004
Reconfigurable LPV control design for Boeing 747-100/200 longitudinal axis
S Ganguli, A Marcos, G Balas
Proceedings of the 2002 American control conference (IEEE cat. no. CH37301 …, 2002
1632002
An application of H∞ fault detection and isolation to a transport aircraft
A Marcos, S Ganguli, GJ Balas
Control Engineering Practice 13 (1), 105-119, 2005
1572005
Fault reconstruction using a LPV sliding mode observer for a class of LPV systems
H Alwi, C Edwards, A Marcos
Journal of the Franklin Institute 349 (2), 510-530, 2012
1042012
Linear parameter varying modeling of the Boeing 747-100/200 longitudinal motion
A Marcos, G Balas
AIAA Guidance, Navigation, and Control Conference and Exhibit, 4347, 2001
982001
A robust integrated controller/diagnosis aircraft application
A Marcos, GJ Balas
International Journal of Robust and Nonlinear Control: IFAC‐Affiliated …, 2005
892005
Linear paramater-varying detection filter design for a boeing 747-100/200 aircraft
I Szászi, A Marcos, GJ Balas, J Bokor
Journal of guidance, control, and dynamics 28 (3), 461-470, 2005
862005
An overview of the FP7 RECONFIGURE project: industrial, scientific and technological objectives
P Goupil, J Boada-Bauxell, A Marcos, P Rosa, M Kerr, L Dalbies
IFAC-PapersOnLine 48 (21), 976-981, 2015
712015
AIRBUS efforts towards advanced real-time fault diagnosis and fault tolerant control
P Goupil, J Boada-Bauxell, A Marcos, E Cortet, M Kerr, H Costa
IFAC Proceedings Volumes 47 (3), 3471-3476, 2014
712014
A Boeing 747-100/200 aircraft fault tolerant and fault diagnostic benchmark
A Marcos, GJ Balas
University of Minnesota, Minneapolis, MN, Technical Report AEM-UoM-2003-1, 2003
692003
Guidance of reusable launchers: improving descent and landing performance
P Simplício, A Marcos, S Bennani
Journal of Guidance, Control, and Dynamics 42 (10), 2206-2219, 2019
562019
Reusable launchers: development of a coupled flight mechanics, guidance, and control benchmark
P Simplício, A Marcos, S Bennani
Journal of Spacecraft and Rockets 57 (1), 74-89, 2020
542020
Advanced diagnosis for sustainable flight guidance and control: The European ADDSAFE project
P Goupil, A Marcos
SAE technical paper, 2011
542011
Structured singular-value analysis of the VEGA launcher in atmospheric flight
P Simplicio, S Bennani, A Marcos, C Roux, X Lefort
Journal of Guidance, Control, and Dynamics 39 (6), 1342-1355, 2016
532016
The European ADDSAFE project: Industrial and academic efforts towards advanced fault diagnosis
P Goupil, A Marcos
Control Engineering Practice 31, 109-125, 2014
522014
Robustness analysis of a reusable launch vehicle flight control law
PP Menon, I Postlethwaite, S Bennani, A Marcos, DG Bates
Control Engineering Practice 17 (7), 751-765, 2009
422009
Flight control design for a highly flexible flutter demonstrator
T Luspay, D Ossmann, M Wuestenhagen, D Teubl, T Baár, M Pusch, ...
AIAA Scitech 2019 Forum, 1817, 2019
372019
LPV modeling, analysis and design in space systems: Rationale, objectives and limitations
A Marcos, S Bennani
AIAA guidance, navigation, and control conference, 5633, 2009
372009
Industrial benchmarking and evaluation of ADDSAFE FDD designs
P Goupil, A Marcos
IFAC Proceedings Volumes 45 (20), 1131-1136, 2012
362012
Review of guidance techniques for landing on small bodies
P Simplício, A Marcos, E Joffre, M Zamaro, N Silva
Progress in Aerospace Sciences 103, 69-83, 2018
352018
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