DISCLAIMER
When possible the pre-prints of the articles have been posted in this site to support academic open access dissemination. This does not waive any rights in copyright of the articles' corresponding authors or publishing organizations.
When possible the pre-prints of the articles have been posted in this site to support academic open access dissemination. This does not waive any rights in copyright of the articles' corresponding authors or publishing organizations.
SW1. [v1.1, 05-Feb-2019, Andrea Iannelli] Software from [J25] "Robust estimations of the region of attraction using invariant sets" article. ZIP
Also available at Github
Also available at Github
BC01. Marcos, A., Bates, D., Postlethwaite, I., “Nonlinear symbolic LFT tools for modeling, analysis and design,” chapter 5 in Nonlinear Analysis and Synthesis Techniques in Aircraft Control, Lecture Notes in Control and Information Science, Springer-Verlag, 2007. PDF
BC02. Biannic, J.M., Marcos, A., Bates, D., Postlethwaite, I., “Nonlinear LFT modeling for on-ground transport aircraft,” chapter 6 in Nonlinear Analysis and Synthesis Techniques in Aircraft Control, Lecture Notes in Control and Information Science, Springer-Verlag, 2007. PDF
BC03. Menon, P.P., Marcos, A., Bennani, S., Postlethwaite, I., Bates, D.G., “Worst-Case Analysis of Control Laws for Re-Entry Vehicles using Hybrid Differential Evolution”, chapter 14 in Advances in Differential Evolution, pp. 319-333, Chakraborty U.K. (eds), Studies in Computational Intelligence, Vol. 143, Springer, Berlin, Heidelberg, 2008.
BC04. Goupil, P., Marcos, A., “Industrial perspectives for aerospace applications,” chapter 19 in GARTEUR FM-AG16, Lecture Notes in Control and Information Science, Springer-Verlag, 2010.
BC05. Marcos, A., Bennani, S., “A Linear Parameter Varying Controller for a Re-entry Vehicle Benchmark,” chapter 2 in Advances in Aerospace Guidance, Navigation and Control, Editors Florian Holzapfel and Stephan Theil, Springer-Verlag, 2011.
BC06. Iannelli, A., Marcos, A., Lowenberg, M., “Limit Cycle Oscillation Amplitude Tailoring based on Describing Function and Singular Structured Analysis,” chapter 6 (pp. 101-119) in Advances in Aerospace Guidance, Navigation and Control, Editors Dolega, B., Glebocki, R., Kordos, D., Zugaj, M., Springer-Verlag, 2017. ISBN 978-3-319-65283-2
BC02. Biannic, J.M., Marcos, A., Bates, D., Postlethwaite, I., “Nonlinear LFT modeling for on-ground transport aircraft,” chapter 6 in Nonlinear Analysis and Synthesis Techniques in Aircraft Control, Lecture Notes in Control and Information Science, Springer-Verlag, 2007. PDF
BC03. Menon, P.P., Marcos, A., Bennani, S., Postlethwaite, I., Bates, D.G., “Worst-Case Analysis of Control Laws for Re-Entry Vehicles using Hybrid Differential Evolution”, chapter 14 in Advances in Differential Evolution, pp. 319-333, Chakraborty U.K. (eds), Studies in Computational Intelligence, Vol. 143, Springer, Berlin, Heidelberg, 2008.
BC04. Goupil, P., Marcos, A., “Industrial perspectives for aerospace applications,” chapter 19 in GARTEUR FM-AG16, Lecture Notes in Control and Information Science, Springer-Verlag, 2010.
BC05. Marcos, A., Bennani, S., “A Linear Parameter Varying Controller for a Re-entry Vehicle Benchmark,” chapter 2 in Advances in Aerospace Guidance, Navigation and Control, Editors Florian Holzapfel and Stephan Theil, Springer-Verlag, 2011.
BC06. Iannelli, A., Marcos, A., Lowenberg, M., “Limit Cycle Oscillation Amplitude Tailoring based on Describing Function and Singular Structured Analysis,” chapter 6 (pp. 101-119) in Advances in Aerospace Guidance, Navigation and Control, Editors Dolega, B., Glebocki, R., Kordos, D., Zugaj, M., Springer-Verlag, 2017. ISBN 978-3-319-65283-2
** The DOI are active links to the official publication site **
J01. Marcos, A., Balas, G.J., “Development of Linear Parameter Varying Models for Aircraft,” AIAA Journal of Guidance, Control, and Dynamics, March 2004, vol. 27, no. 2, pp. 218-228. DOI 10.2514/1.9165 PDF
J02. Marcos, A., Ganguli, S., Balas, G.J., “An Application of H-infinity Fault Detection and Isolation to a Transport Aircraft,” Control Engineering Practice, January 2005, vol. 13, no. 1, pp. 105-119. DOI 10.1016/j.conengprac.2004.02.006. PDF
J03. Szászi, I., Marcos, A., Balas, G.J., Bokor, J., “LPV Detection Filter Design for a Boeing 747-100/200 Aircraft,” AiAA Journal Guidance, Control and Dynamics, June 2005, vol.28, no.3, pp.461-470. DOI 10.2514/1.6689. PDF
J04. Marcos, A., Balas, G.J., “A robust integrated controller/diagnosis aircraft application,” International Journal of Robust and Nonlinear Control, August 2005, vol. 15, no. 12, pp. 531-551. DOI: 10.1002/rnc.1010. PDF
J05. Marcos, A., Bates, D., Postlethwaite, I., “A Symbolic Matrix Decomposition Algorithm for Reduced Order Linear Fractional Transformation Modeling,” IFAC Automatica, July 2007, vol. 43, no. 7, pp. 1125-1306. DOI 10.1016/j.automatica.2006.12.031. PDF
J06. Marcos, A., Turner, M.C., Postlethwaite, I., “An Architecture for Design and Analysis of High-Performance Robust Anti-Windup Compensators,” IEEE Transactions on Automatic Control, September 2007, vol. 52, no. 9, pp. 1672-1679. DOI 10.1109/TAC.2007.904276. PDF
J07. Menon, P.P, Postlethwaite, I., Marcos, A., S. Bennani, S., Bates, D. G., “Robustness Analysis of a Reusable Launch Vehicle Flight Control Law,” Control Engineering Practice, July 2009, vol. 17(7), pp. 751-765. DOI 10.1016/j.conengprac.2008.12.002 .
J08. Szabó, Z., Marcos, A., Mostaza, D., Kerr, M., Rödönyi, G., Bokor, J., Bennani, S., “Development of an Integrated LPV/LFT Framework: Modeling and Data-based Validation Tool,” IEEE Control System Technologies, January 2011, vol. 19, no. 1, pp.104-117. DOI 10.1109/TCST.2010.2072783. PDF
J09. Alwi, H., Edwards, C., Marcos, A., “Fault Reconstruction Using a LPV Sliding Mode Observer for a Class of LPV Systems,” Journal of Franklin Institute, March 2012, vol. 349, No. 2, pp. 510-530. DOI 10.1016/j.jfranklin.2011.06.026. PDF
J10. Goupil, P., Marcos, A., “The European ADDSAFE project: Industrial and academic efforts towards advanced fault diagnosis,” Control Engineering Practice, October 2014, vol. 31. pp.109-125. DOI 10.1016/j.conengprac.2014.03.011. PDF
J11. Edwards, C., Marcos, A., Balas, G., “Special issue on linear parameter varying systems,” (editorial) International Journal of Robust and Nonlinear Control, September 2014, vol. 14, no. 25, pp. 1925-1926. DOI 10.1002/rnc.3228 PDF
J12. Varga, A., Goupil, P., Marcos, A., “CEP special section issue on advanced fault diagnosis for sustainable flight control-The European ADDSAFE project,” (editorial) Control Engineering Practice, October 2014, vol. 31, pp. 107-108. doi.org/10.1016/j.conengprac.2014.06.001 PDF
J13. Marcos, A., Rosa, P., Roux, C., Bartolini, M., Bennani, S., “An overview of the RFCS project V&V framework: optimization‑based and linear tools for worst‑case search,” CEAS Space Journal, June 2015, vol. 7, Issue 2, pp 303-318. DOI 10.1007/s12567-015-0092-2. PDF
J14. Simplício, P., Bennani, S., Lefort, X., Marcos, A., Roux, C, “Structured Singular Value Analysis of the VEGA Launcher in Atmospheric Flight,” AIAA Journal of Guidance, Control, and Dynamics, June 2016, vol. 39, No. 6, pp. 1342-1355. DOI: 10.2514/1.G000335 PDF
J15. Iannelli, A., Marcos, A., Lowenberg, M., “Aeroelastic modeling and stability analysis: a robust approach to the flutter problem,” International Journal of Robust and Nonlinear Control, January 2018, vol. 28, Issue 1, pp. 342-364. DOI: 10.1002/rnc.3878 PDF
J16. Sato. M., Hardier, G., Ferreres, G., Edwards, C., Alwi, H., Chen, L., Marcos, A., "Fault Tolerance - Background and Recent Trends,” Journal of the Society of Instrument and Control Engineers (SICE), April 2018, Vol. 57, No. 4, pp. 279-286. DOI: 10.11499/sicejl.57.279 PDF
J17. Iannelli, A., Marcos, A., Lowenberg, M., “Study of Flexible Aircraft Body Freedom Flutter with Robustness Tools,” AIAA Journal of Guidance, Control and Dynamics, May 2018, vol. 41, No. 5, pp. 1083-1094. DOI: 10.2514/1.G003165, PDF
J18. Simplício, P., Marcos, A., Joffre, E., Zamaro, M., Silva, N., “Synthesis and Analysis of Robust Control Compensators for Space Descent & Landing,” International Journal of Robust and Nonlinear Control, September 2018, vol. 28, no. 13, pp. 3871-3892. DOI: 10.1002/rnc.4109, PDF
J19. Joffre, E., Zamaro, M., Silva, N., Marcos, A., Simplício, P., Richardson, B., "Trajectory Design and Guidance for Landing on Phobos,” Acta Astronautica, October 2018, vol. 151, pp. 389-400. DOI: 10.1016/j.actaastro.2018.06.024, PDF
J20. Simplício, P., Marcos, A., Joffre, E., Zamaro, M., Silva, N., "Review of Guidance Techniques of Landing on Small Bodies,” Progress in Aerospace Sciences, , November 2018, vol.103, pp. 69-83. DOI:10.1016/j.paerosci.2018.10.005, PDF
J21. Tong, L., Marcos, A., Zhang, S., "Enhanced disturbance rejection control based test rocket control system design and validation,” ISA Transactions, January 2019, vol.84, pp.31-42. DOI:10.1016/j.isatra.2018.08.023
J22. Iannelli, A., Marcos, A., Lowenberg, M., “Nonlinear robust approaches to study stability and post-critical behaviour of an aeroelastic plant,” IEEE Transactions on Control Systems Technology, March 2019, Vol. 27, Issue 2, pp. 703-716. DOI:10.1109/TCST.2017.2779110, PDF
J23. Simplício, P., Marcos, A., Joffre, E., Zamaro, M., Silva, N., "Systematic Performance-Oriented Guidance Tuning for Descent & Landing on Small Planetary Bodies,” Acta Astronautica, May 2019, vol. 158, pp.44-54. DOI:10.1016/j.actaastro.2018.07.028, PDF
J24. Iannelli, A., Marcos, A., Lowenberg, M., "Robust estimations of the region of attraction using invariant sets," Journal of the Franklin Institute: Engineering and Applied Mathematics, May 2019, vol. 356, Issue 8, pp. 4622-4647, See also SW1 in Software section, DOI:10.1016/j.jfranklin.2019.02.013 PDF
J25. Iannelli, A., Seiler, P., Marcos, A., “Worst-case Disturbances for Time-Varying Systems with Application to Flexible Aircraft,” AIAA Journal of Guidance, Control and Dynamics, June 2019, vol. 42, issue 6, pp. 1261-1271. DOI:10.2514/1.G004023, PDF
J26. Navarro-Tapia, D., Marcos, A., Simplício, P., Bennani, S., Roux, C., "Legacy Recovery and Robust Augmentation Structured Design for the VEGA Launcher," International Journal of Robust and Nonlinear Control, July 2019, vol. 29, Issue 11, pp. 3363-3388. DOI: 10.1002/rnc.4557 PDF
J27. Iannelli, A., Seiler, P., Marcos, A., "Region of Attraction Analysis with Integral Quadratic Constraints," IFAC Automatica, November 2019, vol. 109. DOI: 10.1016/j.automatica.2019.108543 PDF
J28. Simplício, P., Marcos, A., Bennani, S., “Guidance of Reusable Launchers: Improving Descent and Landing Performance,” AIAA Journal of Guidance, Control, and Dynamics, October 2019, vol. 42, Issue 10. DOI: 10.2514/1.G004155 PDF
J29. Simplício, P., Marcos, A., Bennani, S., “Reusable Launchers: Development of a Coupled Flight Mechanics, Guidance and Control Benchmark,” AIAA Journal of Space and Rockets, January 2020, vol. 57, Issue 1, pp. 74–89. DOI: 10.2514/1.A34429 PDF
J30. Waitman, S., Marcos, A., “H-infinity control design for active flutter suppression of flexible-wing UAV demonstrator,” AIAA Journal of Guidance, Control, and Dynamics, April 2020, vol. 43, issue 4, pp. 656-672. DOI: 10.2514/1.G004618 PDF
J31. Marcos, A., Navarro-Tapia, D., Simplício, P., Bennani, S., “Robust Control for Launchers: VEGA study case,” Journal of the Society of Instrument and Control Engineers (SICE), March 2020, Vol. 59, no. 3, pp. 192-202. DOI: 10.11499/sicejl.59.192 PDF
J32. Iannelli, A., Marcos, A., Bombardieri, R., Cavallaro, R., “Linear Fractional Transformation co-modeling of high-order aeroelastic systems for robust flutter analysis,” European Journal of Control, July 2020, Vol. 54, pp. 49-63. DOI: 10.1016/j.ejcon.2019.12.002 PDF
J33. Iannelli, A., Lowenberg, M., Marcos, A., "Computation of bifurcation margins based on robust control concepts," SIAM Journal on Applied Dynamics Systems, September 2020, vol.19, no.3, pp.1956-1992. DOI: 10.1137/19M1303678 PDF
J34. Iannelli, A., Lowenberg, M., Marcos, A., "An extension of the structured singular value to nonlinear systems with application to robust flutter analysis," CEAS Aeronautical Journal, December 2020, vol. 11, issue. 4, pp. 1057-1069, open access, DOI: 10.1007/s13272-020-00469-4 PDF
J35. Iannelli, A., Lowenberg, M., Marcos, A., "On the effect of the model uncertainty on the Hopf bifurcation of aeroelastic systems," Nonlinear Dynamics, February 2021, open access, DOI: 10.1007/s11071-020-06169-2 PDF
J36. Navarro-Tapia, D., Marcos, A., Bennani, S., "Envelope Extension via Adaptive Augmented Thrust Vector Control System," AIAA Journal of Guidance, Control, and Dynamics, May 2021, vol. 44, number 5, pp. 1044-1052, DOI: 10.2514/1.G005436 PDF
J37. Simplício, P., Marcos, A., Bennani, S., “Launcher Flight Control Design using Robust Wind Disturbance Observation,” Acta Astronautica, September 2021, vol. 186, pp. 303-318, DOI: 10.1016/j.actaastro.2021.05.044
J38.Marcos, A., Waitman, S., Sato, M., "Fault Tolerant Linear Parameter Varying Flight Control Design, Verification and Validation," Journal of the Franklin Institute, January 2022, vol. 359, no. 2, pp.653-676, DOI: 10.1016/j.jfranklin.2021.02.040
J39. Navarro-Tapia, D., Marcos, A., Bennani, S., "The VEGA launcher atmospheric control problem: a case for linear parameter varying synthesis," Journal of the Franklin Institute, January 2022, vol. 359, no. 2, pp.899-927, DOI: 10.1016/j.jfranklin.2021.07.057
J02. Marcos, A., Ganguli, S., Balas, G.J., “An Application of H-infinity Fault Detection and Isolation to a Transport Aircraft,” Control Engineering Practice, January 2005, vol. 13, no. 1, pp. 105-119. DOI 10.1016/j.conengprac.2004.02.006. PDF
J03. Szászi, I., Marcos, A., Balas, G.J., Bokor, J., “LPV Detection Filter Design for a Boeing 747-100/200 Aircraft,” AiAA Journal Guidance, Control and Dynamics, June 2005, vol.28, no.3, pp.461-470. DOI 10.2514/1.6689. PDF
J04. Marcos, A., Balas, G.J., “A robust integrated controller/diagnosis aircraft application,” International Journal of Robust and Nonlinear Control, August 2005, vol. 15, no. 12, pp. 531-551. DOI: 10.1002/rnc.1010. PDF
J05. Marcos, A., Bates, D., Postlethwaite, I., “A Symbolic Matrix Decomposition Algorithm for Reduced Order Linear Fractional Transformation Modeling,” IFAC Automatica, July 2007, vol. 43, no. 7, pp. 1125-1306. DOI 10.1016/j.automatica.2006.12.031. PDF
J06. Marcos, A., Turner, M.C., Postlethwaite, I., “An Architecture for Design and Analysis of High-Performance Robust Anti-Windup Compensators,” IEEE Transactions on Automatic Control, September 2007, vol. 52, no. 9, pp. 1672-1679. DOI 10.1109/TAC.2007.904276. PDF
J07. Menon, P.P, Postlethwaite, I., Marcos, A., S. Bennani, S., Bates, D. G., “Robustness Analysis of a Reusable Launch Vehicle Flight Control Law,” Control Engineering Practice, July 2009, vol. 17(7), pp. 751-765. DOI 10.1016/j.conengprac.2008.12.002 .
J08. Szabó, Z., Marcos, A., Mostaza, D., Kerr, M., Rödönyi, G., Bokor, J., Bennani, S., “Development of an Integrated LPV/LFT Framework: Modeling and Data-based Validation Tool,” IEEE Control System Technologies, January 2011, vol. 19, no. 1, pp.104-117. DOI 10.1109/TCST.2010.2072783. PDF
J09. Alwi, H., Edwards, C., Marcos, A., “Fault Reconstruction Using a LPV Sliding Mode Observer for a Class of LPV Systems,” Journal of Franklin Institute, March 2012, vol. 349, No. 2, pp. 510-530. DOI 10.1016/j.jfranklin.2011.06.026. PDF
J10. Goupil, P., Marcos, A., “The European ADDSAFE project: Industrial and academic efforts towards advanced fault diagnosis,” Control Engineering Practice, October 2014, vol. 31. pp.109-125. DOI 10.1016/j.conengprac.2014.03.011. PDF
J11. Edwards, C., Marcos, A., Balas, G., “Special issue on linear parameter varying systems,” (editorial) International Journal of Robust and Nonlinear Control, September 2014, vol. 14, no. 25, pp. 1925-1926. DOI 10.1002/rnc.3228 PDF
J12. Varga, A., Goupil, P., Marcos, A., “CEP special section issue on advanced fault diagnosis for sustainable flight control-The European ADDSAFE project,” (editorial) Control Engineering Practice, October 2014, vol. 31, pp. 107-108. doi.org/10.1016/j.conengprac.2014.06.001 PDF
J13. Marcos, A., Rosa, P., Roux, C., Bartolini, M., Bennani, S., “An overview of the RFCS project V&V framework: optimization‑based and linear tools for worst‑case search,” CEAS Space Journal, June 2015, vol. 7, Issue 2, pp 303-318. DOI 10.1007/s12567-015-0092-2. PDF
J14. Simplício, P., Bennani, S., Lefort, X., Marcos, A., Roux, C, “Structured Singular Value Analysis of the VEGA Launcher in Atmospheric Flight,” AIAA Journal of Guidance, Control, and Dynamics, June 2016, vol. 39, No. 6, pp. 1342-1355. DOI: 10.2514/1.G000335 PDF
J15. Iannelli, A., Marcos, A., Lowenberg, M., “Aeroelastic modeling and stability analysis: a robust approach to the flutter problem,” International Journal of Robust and Nonlinear Control, January 2018, vol. 28, Issue 1, pp. 342-364. DOI: 10.1002/rnc.3878 PDF
J16. Sato. M., Hardier, G., Ferreres, G., Edwards, C., Alwi, H., Chen, L., Marcos, A., "Fault Tolerance - Background and Recent Trends,” Journal of the Society of Instrument and Control Engineers (SICE), April 2018, Vol. 57, No. 4, pp. 279-286. DOI: 10.11499/sicejl.57.279 PDF
J17. Iannelli, A., Marcos, A., Lowenberg, M., “Study of Flexible Aircraft Body Freedom Flutter with Robustness Tools,” AIAA Journal of Guidance, Control and Dynamics, May 2018, vol. 41, No. 5, pp. 1083-1094. DOI: 10.2514/1.G003165, PDF
J18. Simplício, P., Marcos, A., Joffre, E., Zamaro, M., Silva, N., “Synthesis and Analysis of Robust Control Compensators for Space Descent & Landing,” International Journal of Robust and Nonlinear Control, September 2018, vol. 28, no. 13, pp. 3871-3892. DOI: 10.1002/rnc.4109, PDF
J19. Joffre, E., Zamaro, M., Silva, N., Marcos, A., Simplício, P., Richardson, B., "Trajectory Design and Guidance for Landing on Phobos,” Acta Astronautica, October 2018, vol. 151, pp. 389-400. DOI: 10.1016/j.actaastro.2018.06.024, PDF
J20. Simplício, P., Marcos, A., Joffre, E., Zamaro, M., Silva, N., "Review of Guidance Techniques of Landing on Small Bodies,” Progress in Aerospace Sciences, , November 2018, vol.103, pp. 69-83. DOI:10.1016/j.paerosci.2018.10.005, PDF
J21. Tong, L., Marcos, A., Zhang, S., "Enhanced disturbance rejection control based test rocket control system design and validation,” ISA Transactions, January 2019, vol.84, pp.31-42. DOI:10.1016/j.isatra.2018.08.023
J22. Iannelli, A., Marcos, A., Lowenberg, M., “Nonlinear robust approaches to study stability and post-critical behaviour of an aeroelastic plant,” IEEE Transactions on Control Systems Technology, March 2019, Vol. 27, Issue 2, pp. 703-716. DOI:10.1109/TCST.2017.2779110, PDF
J23. Simplício, P., Marcos, A., Joffre, E., Zamaro, M., Silva, N., "Systematic Performance-Oriented Guidance Tuning for Descent & Landing on Small Planetary Bodies,” Acta Astronautica, May 2019, vol. 158, pp.44-54. DOI:10.1016/j.actaastro.2018.07.028, PDF
J24. Iannelli, A., Marcos, A., Lowenberg, M., "Robust estimations of the region of attraction using invariant sets," Journal of the Franklin Institute: Engineering and Applied Mathematics, May 2019, vol. 356, Issue 8, pp. 4622-4647, See also SW1 in Software section, DOI:10.1016/j.jfranklin.2019.02.013 PDF
J25. Iannelli, A., Seiler, P., Marcos, A., “Worst-case Disturbances for Time-Varying Systems with Application to Flexible Aircraft,” AIAA Journal of Guidance, Control and Dynamics, June 2019, vol. 42, issue 6, pp. 1261-1271. DOI:10.2514/1.G004023, PDF
J26. Navarro-Tapia, D., Marcos, A., Simplício, P., Bennani, S., Roux, C., "Legacy Recovery and Robust Augmentation Structured Design for the VEGA Launcher," International Journal of Robust and Nonlinear Control, July 2019, vol. 29, Issue 11, pp. 3363-3388. DOI: 10.1002/rnc.4557 PDF
J27. Iannelli, A., Seiler, P., Marcos, A., "Region of Attraction Analysis with Integral Quadratic Constraints," IFAC Automatica, November 2019, vol. 109. DOI: 10.1016/j.automatica.2019.108543 PDF
J28. Simplício, P., Marcos, A., Bennani, S., “Guidance of Reusable Launchers: Improving Descent and Landing Performance,” AIAA Journal of Guidance, Control, and Dynamics, October 2019, vol. 42, Issue 10. DOI: 10.2514/1.G004155 PDF
J29. Simplício, P., Marcos, A., Bennani, S., “Reusable Launchers: Development of a Coupled Flight Mechanics, Guidance and Control Benchmark,” AIAA Journal of Space and Rockets, January 2020, vol. 57, Issue 1, pp. 74–89. DOI: 10.2514/1.A34429 PDF
J30. Waitman, S., Marcos, A., “H-infinity control design for active flutter suppression of flexible-wing UAV demonstrator,” AIAA Journal of Guidance, Control, and Dynamics, April 2020, vol. 43, issue 4, pp. 656-672. DOI: 10.2514/1.G004618 PDF
J31. Marcos, A., Navarro-Tapia, D., Simplício, P., Bennani, S., “Robust Control for Launchers: VEGA study case,” Journal of the Society of Instrument and Control Engineers (SICE), March 2020, Vol. 59, no. 3, pp. 192-202. DOI: 10.11499/sicejl.59.192 PDF
J32. Iannelli, A., Marcos, A., Bombardieri, R., Cavallaro, R., “Linear Fractional Transformation co-modeling of high-order aeroelastic systems for robust flutter analysis,” European Journal of Control, July 2020, Vol. 54, pp. 49-63. DOI: 10.1016/j.ejcon.2019.12.002 PDF
J33. Iannelli, A., Lowenberg, M., Marcos, A., "Computation of bifurcation margins based on robust control concepts," SIAM Journal on Applied Dynamics Systems, September 2020, vol.19, no.3, pp.1956-1992. DOI: 10.1137/19M1303678 PDF
J34. Iannelli, A., Lowenberg, M., Marcos, A., "An extension of the structured singular value to nonlinear systems with application to robust flutter analysis," CEAS Aeronautical Journal, December 2020, vol. 11, issue. 4, pp. 1057-1069, open access, DOI: 10.1007/s13272-020-00469-4 PDF
J35. Iannelli, A., Lowenberg, M., Marcos, A., "On the effect of the model uncertainty on the Hopf bifurcation of aeroelastic systems," Nonlinear Dynamics, February 2021, open access, DOI: 10.1007/s11071-020-06169-2 PDF
J36. Navarro-Tapia, D., Marcos, A., Bennani, S., "Envelope Extension via Adaptive Augmented Thrust Vector Control System," AIAA Journal of Guidance, Control, and Dynamics, May 2021, vol. 44, number 5, pp. 1044-1052, DOI: 10.2514/1.G005436 PDF
J37. Simplício, P., Marcos, A., Bennani, S., “Launcher Flight Control Design using Robust Wind Disturbance Observation,” Acta Astronautica, September 2021, vol. 186, pp. 303-318, DOI: 10.1016/j.actaastro.2021.05.044
J38.Marcos, A., Waitman, S., Sato, M., "Fault Tolerant Linear Parameter Varying Flight Control Design, Verification and Validation," Journal of the Franklin Institute, January 2022, vol. 359, no. 2, pp.653-676, DOI: 10.1016/j.jfranklin.2021.02.040
J39. Navarro-Tapia, D., Marcos, A., Bennani, S., "The VEGA launcher atmospheric control problem: a case for linear parameter varying synthesis," Journal of the Franklin Institute, January 2022, vol. 359, no. 2, pp.899-927, DOI: 10.1016/j.jfranklin.2021.07.057
- Marcos, A., Rodríguez, J., “Preliminary Identification of Buffet Problems in High Speed Civil Transport,” AIAA Region V Student Conference, St. Louis, Missouri, USA, April 1997.
- Marcos, A., Balas, G.J., “Linear Parameter Varying Modeling of the Boeing 747-100/200 Longitudinal Motion,” AIAA GNC Conference, AIAA-2001-4347. Montreal, Canada, August 2001 PDF
- Ganguli, S., Marcos, A., Balas, G.J., “Reconfigurable LPV Control Design for B-747-100/200 Longitudinal Axis,” American Control Conference, Anchorage, Alaska, USA, May 2002 PDF
- Szászi, I., Ganguli, S., Marcos, A., Balas, G.J., Bokor, J., “Application of FDI to a Nonlinear Boeing-747 Aircraft,” Mediterranean Conference on Control and Automation, Lisbon, Portugal, July 2002 PDF
- Szászi, I., Marcos, A., Balas, G.J., Bokor, J., “LPV Detection Filter Design for Boeing 747-100/200,” AIAA GNC Conference, AIAA-2002-4957. Monterey, USA, August 2002 PDF
- Marcos, A., Ganguli, S., Balas, G.J., “Application of H-infinity Fault Detection and Isolation to a Boeing 747-100/200,” AIAA GNC Conference, AIAA-2002-4944. Monterey, California, USA, August 2002 PDF
- Marcos, A., Ganguli, S., Balas, G.J., “New Strategies for Fault Tolerant Control and Fault Diagnostic,” IFAC SAFEPROCESS’03, Washington, D.C., USA, June 2003 PDF
- Ghaffari, A., Ghasemi, F., Marcos, A., “Identification of a Boeing 747-100/200 Longitudinal Motion Using Neural Networks,” The Second International & The Fifth National Conference of Iranian Aerospace Society, Isfahan, Iran, February 2004.
- Marcos A., Balas, G.J., Mylaraswamy D., “Robust Identification and Residual Generation Application to a Turbofan Engine,” IEEE Aerospace Conference, Big Sky, Montana, March 2004 PDF
- Marcos A., Balas, G.J., “Linear Fractional Transformation Formulation of the Integrated Controller Approach,” Control 2004 Conference UKACC, Bath, UK, September 2004 PDF
- Marcos, A., Bates, D., Postlethwaite, I., “Flight Dynamics Application of a New Symbolic Matrix Order-Reduction Algorithm,” International Conference on Polynomial System Solving, Paris, FR, Nov. 2004 PDF
- Marcos, A., Bates, D., Postlethwaite, I. “Exact Nonlinear Modeling Using Symbolic Linear Fractional Transformations,” IFAC World Congress, Prague, Czech Republic, July 2005. DOI 10.3182/20050703-6-CZ-1902.00032 PDF
- Marcos, A., Bates, D., Postlethwaite, I. “A Multivariate Polynomial Matrix Order-Reduction Algorithm for Linear Fractional Transformation Modeling,” IFAC World Congress, Prague, Czech Rep., July 2005. DOI 10.3182/20050703-6-CZ-1902.00999 PDF
- Marcos, A., Mylaraswamy, D., Balas, G.J., “Robust Model Identification Application to a Turbofan Engine,” IFAC World Congress, Prague, Czech Republic, July 2005. DOI 10.3182/20050703-6-CZ-1902.00148 PDF
- Marcos, A., Balas, G.J., Bokor, J., “Integrated FDI and Control for Transport Aircraft,” AIAA GNC Conference, AIAA-2005-5937. San Francisco, California, USA, August 2005 PDF
- Marcos, A., Balas, G.J. “Nested Integrated Control and Diagnostic Filter Design,” 44th IEEE CDC-ECC 2005, Seville, Spain, December 2005 PDF
- Marcos, A., Bates, D., Postlethwaite, I. “Control oriented uncertainty modeling using µ sensitivities and skewed µ analysis tool,” 44th IEEE CDC-ECC 2005, Seville, Spain, December 2005 PDF
- Marcos, A., Biannic, J.M., Jeanneau, M., Bates, D., Postlethwaite, I. “Aircraft modeling for nonlinear and robust control design and analysis,” 5th IFAC Symposium on Robust Control Design 2006, Toulouse, France, July 2006 PDF
- Marcos, A., Turner, M., Bates, D., Postlethwaite, I. “Robustification of static and low order anti-windup designs,” 5th IFAC Symposium on Robust Control Design 2006, Toulouse, France, July 2006 PDF
- Marcos, A., Turner, M., Postlethwaite, I. “High-performance Architecture for Design and Analysis of Robust Anti-Windup Compensator,” American Control Conference 2006, Minneapolis, USA PDF
- Castro, H., Bennani, S., Marcos, A., “Robust Filter Design for a Re-Entry Vehicle,” 7th International Conference on Dynamics and Control of Systems and Structure in Space 2006, Greenwich, England PDF
- Biannic, J.M., Marcos, A., Jeanneau, M. “Nonlinear simplified LFT modeling of an aircraft on ground,” IEEE International Conference on Control Application 2006, Munich, Germany PDF
- Castro, H., Bennani, S., Marcos, A., “Integrated vs. Decoupled Fault Detection Filter & Flight Control Law Designs for a Re-Entry Vehicle,” IEEE International Conference on Control Application 2006, Munich, Germany PDF
- Marcos, A., Peñín, L.F., Caramagno, A., Sommer, J., Belau, W., “Atmospheric Re-Entry NDI Control Design for the Hopper RLV Concept,” 17th IFAC Symposium on Automatic Control in Aerospace, Toulouse, FR, June 2007 PDF
- Menon, P.P, Bates, D.G., Postlethwaite, I., Marcos, A., Vicente, F., Bennani, S., “Worst-Case Analysis of Flight Control Laws for Re-Entry Vehicles,” 17th IFAC Symposium on Automatic Control in Aerospace, Toulouse, FR, June 2007 PDF
- Marcos, A., Peñín, L.F., DiSotto, E., Drai, R., “Formation Flying Control in Highly Elliptical Orbits,” AIAA GNC Conference, Hilton Head, South Carolina, USA. August 2007 PDF
- Di Sotto, E., Peñín, L.F., Bastante, J.C., Marcos, A., Branco, J., “FF Analysis and GNC Concept for a FF Mission in Highly Eccentric Orbit,” 3rd International Symposium on Formation Flying, Missions and Technologies, Noordwijk, ESA-ESTEC, April 2008 PDF
- Marcos, A., De Zaiacomo, G., Peñín, L.F., Bornschlegl, E., “Fault Analysis for Robust FDI Design During RLV Ascent and Re-entry Phases,” 7th International ESA Conference on Guidance, Navigation & Control Systems, Ireland, June 2008 PDF
- Menon, P.P., Marcos, A., Bennani, S., Postlethwaite, I., Bates, D.G., “Multiobjective Worst-Case Analysis of a Re-Entry Vehicle Control Law”, IFAC World Congress Automatic Control, Korea, 2008. DOI 10.3182/20080706-5-KR-1001.00427
- Marcos, A., De Zaiacomo, G., Peñín, L.F., “Simulation-Based Fault Analysis Methodology for Aerospace Vehicles,” AIAA GNC Conference, Honolulu, USA, August 2008 PDF
- Marcos, A., Peñín, L.F., Caramagno, A., Sommer, J., Belau, W. Bornschlegl, E., “Guidance and Control Design for the Ascent Phase of the Hopper RLV,” AIAA GNC Conference, Honolulu, USA, August 2008 PDF
- Kerr, M.L., Marcos, A., Peñín, L.F., “Gain Scheduled FDI for a Re-entry Vehicle,” AIAA GNC Conference, Honolulu, USA, August 2008 PDF
- Marcos, A., Peñín, L.F., Di Sotto, E., “LFT Modeling for the analysis of relative motion controllers in eccentric orbits,” 2nd IEEE Multi-Conference on Systems and Control (MSC), San Antonio, USA, September 2008. Invited Paper PDF
- Marcos, A., Mostaza, D., Peñín, L.F., “Achievable Moments NDI-based Fault Tolerant Thrust Vector Control of an Atmospheric Vehicle During Ascent,” IFAC SAFEPROCESS’09, Barcelona, Spain, June 2009 PDF
- Kerr, M.L., Marcos, A., Peñín, L.F., “Development of an FDI Filter for the Hopper RLV during Re-entry,” IFAC SAFEPROCESS’09, Barcelona, Spain, June 2009 PDF
- Marcos, A., Bennani, S., “LPV Modeling, Analysis and Design in Space Systems: Rationale, Objectives and Limitations,” AIAA GNC Conference, Chicago, USA, August 2009 PDF
- Marcos, A., Kerr, M.L., De Zaiacomo, G., Peñín, L.F., Szabó, Z., Rödönyi, G., Bokor, J., “Application of LPV/LFT Modeling and Data-based Validation to a re-entry vehicle,” AIAA GNC Conference, Chicago, USA, August 2009 PDF
- Kerr, M.L., Marcos, Peñín, L.F., Brieger, O., Postlethwaite, I., Turner, M., “Piloted Assessment of a Fault Diagnosis Algorithm on the ATTAS Aircraft,” AIAA GNC Conference, Chicago, USA, August 2009 PDF
- Marcos, A., Veenman, J., Scherer, C., De Zaiacomo, G., Mostaza, D., Kerr, M.L., Koroglu, H., Bennani, S., “Application of LPV Modeling, Design and Analysis Methods to a Re-entry Vehicle ,” AIAA GNC Conference, Toronto, Canada, August 2010 PDF
- Kerr, M.L., Marcos, A., Peñín, L.F., “Development and Testing of a GNC-FDI Filter for a Reusable Launch Vehicle during Ascent,” AIAA GNC Conference, Toronto, Canada, August 2010 PDF
- Alwi, H., Edwards, C., Marcos, A., “Actuator and Sensor Faults Reconstruction Using an LPV Sliding Mode Observer,” AIAA GNC Conference, Toronto, Canada, August 2010 PDF
- Marcos, A., “A gain scheduled H-infinity controller for a re-entry benchmark,” AIAA GNC Conference, Toronto, Canada, August 2010 PDF
- Marcos, A., Kerr, M.L., Peñín, L.F., “Application of a Fault Accommodation Approach to a Re-entry Vehicle,” in invited session on “Active Fault Tolerant Control Systems (AFTCS) in Aerospace,” 18th IFAC Symposium on Automatic Control in Aerospace ACA'2010, September, Nara, Japan PDF
- Alwi, H., Edwards, C., Marcos, A., “FDI for a Mars-Orbiting Satellite based on a Sliding Mode Observer Scheme,” IEEE Conference on Control and Fault-Tolerant Systems SYTOL’10, Nice, France PDF
- Marcos, A., “Advanced Fault Diagnosis for Sustainable Flight Guidance and Control,” 6th European Aeronautics Days, Madrid, Spain, March 2011.
- Marcos, A., Bennani, S., “A Linear Parameter Varying Controller for a Re-entry Vehicle Benchmark,” 1st Council of European Aerospace Societies (CEAS) GNC Conference, Munich, Germany, April 2011 PDF
- Peñín, L.F., Marcos, A., Kerr, M., “GNC FDI/FTC Technology For Re-entry Vehicles,” 3rd International Atmospheric Reentry Association (ARA) Conference, Arcachon, France, May 2011.
- Marcos, A., Peñín, L.F., Caramagno, A., Roux, C., Rotunno, M., Joos, D.H., Bennani, S., “The V&V Problematic for Launchers: Current Practice and Potential Advantages on the Application of Modern Analysis Techniques,” 8th ESA GNC Conference, Carlsbad, Czech Republic, June 2011 PDF
- Marcos, A., “Application of H-infinity fault diagnosis to ADDSAFE benchmark: the control surface jamming case,” AIAA GNC Conference, Portland, USA, August 2011 PDF
- Goupil, P., Marcos, A., “Advanced Diagnosis for Sustainable Flight Guidance and Control: The European ADDSAFE Project,” SAE Aerospace Technology Conference and Exposition, 2011. Link
- Marcos, A., Alwi, H., Edwards, C., Falcoz, A., Bornschlegl, E., “Verification & Validation of a Satellite Fault Detection and Isolation Scheme Based on Sliding-Mode Observers,” paper on invited session Fault Detection, Isolation and Reconfiguration in Space at SAFEPROCESS 2012, Mexico. DOI 10.3182/20120829-3-MX-2028.00167 PDF
- Marcos, A., “Assessment on the ADDSAFE Benchmark Simulator of an H-infinity Fault Detection Design for Aircraft,” paper on invited session European efforts towards Advanced Fault Diagnosis: the FP7 ADDSAFE project – Part II at SAFEPROCESS 2012, Mexico. DOI 10.3182/20120829-3-MX-2028.00202 PDF
- Goupil, P., Marcos, A., “Industrial benchmarking and evaluation of ADDSAFE FDD designs,” paper on invited session European efforts towards Advanced Fault Diagnosis: the FP7 ADDSAFE project – Part II at SAFEPROCESS 2012, Mexico. DOI 10.3182/20120829-3-MX-2028.00168 PDF
- García de Marina, H., Marcos, A., Haya, R., “Angle of Attack and True Airspeed failure sensor detection and recovery based on Unscented Kalman Filters for the ALPHA vehicle,” SAFEPROCESS’12, Mexico. DOI 10.3182/20120829-3-MX-2028.00170 PDF
- Pulecchi, T., Marcos, A., Roux, C., Mantini, V., Bennani, S., “Frozen-time and time-varying robust stability certificates for the coupled pitch/yaw motion of an axial-symmetric launch vehicle,” paper on invited session SPACE V&V at ROCOND 2012, Aalborg, Denmark. DOI 10.3182/20120620-3-DK-2025.00111 PDF
- Marcos, A., Peñín, L.F., Le Gonidec, S., Lemaitre, A., “HMS-Control-Interaction Architecture for Rocket Engines,” AIAA GNC 2012, Minneapolis, USA PDF
- Roux, C., Mantini, V., Marcos, A., Peñín, L.F., Bennani, S., “Robust Flight Control System Design Verification & Validation for Launchers,” paper on invited session Robust Launcher Flight Control System Design Verification and Validation special session at AIAA GNC 2012, Minneapolis, USA PDF
- Pulecchi, T., Marcos, A., Roux, C., Mantini, V., Bennani, S., “Thrust Vector Control Robustness of axial-symmetric Launch Vehicles with Fuel Slosh,” paper on invited session Robust Launcher Flight Control System Design Verification and Validation special session at AIAA GNC 2012, Minneapolis, USA PDF
- Marcos, A., García de Marina, H., Mantini, V., Roux, C., Bennani, S., “Optimization-based worst-case analysis of a launcher during the atmospheric ascent phase,” AIAA GNC 2013, Boston, USA PDF
- Marcos, A., Mantini, V., Roux, C., Bennani, S., “Bridging the Gap between Linear and Nonlinear Worst-Case Analysis: An Application Case to the Atmospheric Phase of the VEGA Launcher,” 19th IFAC Symposium on Automatic Control in Aerospace (ACA), Wuerzburg, Germany, 2013 PDF
- Marcos, A., Peñín, L.F., Malikov, D., Reichstadt, S., Le Gonidec, S., “Fault Detection and Isolation for a Rocket Engine Valve,” 19th IFAC Symposium on Automatic Control in Aerospace (ACA), Germany, 2013 PDF
- Marcos, A., Rosa, P., Roux, C., Bartolini, M., Bennani, S., “An overview of the RFCS project V&V framework: optimization-based and linear tools for worst-case search,” 9th International ESA Conference on GNC Systems, Oporto, Portugal, June 2014 PDF
- Marcos, A., Peñín, L.F., Caramagno, A., “Model-Based FDIR: from paper to planes,” paper on invited session Bridging the Gap between Academia and Industry: Successful Aerospace Collaborations, IFAC World Congress, Cape Town, South Africa, August 2014. DOI 10.3182/20140824-6-ZA-1003.01297 PDF
- Goupil, P., Boada-Bauxel, J., Marcos, A., Cortet, E., Kerr, M., Costa, H., “AIRBUS efforts towards advanced real-time Fault Diagnosis and Fault Tolerant Control,” paper on invited session European Efforts towards Advanced Fault Diagnosis and Fault Tolerant Control for Civil Aircraft: The FP7 RECONFIGURE Project, IFAC World Congress, Cape Town, South Africa, August 2014. DOI 10.3182/20140824-6-ZA-1003.01945 PDF
- Valli, M., Spallotta, D., Roux, C., Marcos, A., Mujumdar, A., Menon, P.P., Bennani, S., “Thrust Vector Control Validation Results for Performance and Stability Robustness Assessments,” paper on invited session Worst-case V&V Applications for Aerospace GNC systems - Part I at 3rd CEAS EUROGNC CONFERENCE, Toulouse, France, April 2015 PDF
- Marcos, A., Roux, C., Bennani, S., “Stochastic mu-Analysis for launcher thrust vector control systems,” paper on invited session Worst-case V&V Applications for Aerospace GNC systems - Part 2 at 3rd CEAS EUROGNC CONFERENCE, Toulouse, France, April 2015 PDF
- Marcos, A., Bennani, S., Roux, C., Valli, M., “Uncertainty Modeling and Robust Analysis of Atmospheric Launchers: Incremental Steps for Industrial Transfer,” 8th IFAC Symposium on Robust Control Design (ROCOND), Bratislava, Slovakia, July 2015 doi.org/10.1016/j.ifacol.2015.09.494 PDF
- Goupil, P., Boada-Bauxel, J., Marcos, A., Rosa, P., Kerr, M., Dalbies, L., “An overview of the FP7 RECONFIGURE project: industrial, scientific and technological objectives” paper on invited session on FP7 RECONFIGURE Project: Theoretical and Practical Contributions towards Advanced Real-Time FDD and FTC for Civil Aircraft at SAFEPROCESS 2015, Paris, France, September 2015. doi.org/10.1016/j.ifacol.2015.09.653 PDF
- Marcos, A., Bennani, S., Roux, C., “LPV modeling and LFT Uncertainty Identification for Robust Analysis: application to the VEGA Launcher during Atmospheric Phase,” 1st IFAC Workshop on Linear Parameter Varying Systems, Grenoble, France, October 2015. https://doi.org/10.1016/j.ifacol.2015.11.123 PDF
- Iannelli, A., Marcos, A., Lowenberg, M., "Comparison of Aeroelastic Modeling and Robust Flutter Analysis of a Typical Section," 20th IFAC Symposium on Automatic Control in Aerospace (ACA16), Sherbrook, Canada, August 2016. https://doi.org/10.1016/j.ifacol.2016.09.070 PDF
- Currie, C., Marcos, A., Turnbull, O., "Wind Optimal Flight Trajectories to Minimise Fuel Consumption within a 3 Dimensional Flight Network," 11th UKACC International Conference on Control, (UKACC16), Belfast, UK, September 2016. DOI10.1109/CONTROL.2016.7737600 PDF
- Iannelli, A., Marcos, A., Lowenberg, M., “Modeling and Robust Body Freedom Flutter Analysis of Flexible Aircraft Configurations,” IEEE Multi-Conference on Systems and Control (MSC 2016), Buenos Aires, Argentina, September 2016. DOI10.1109/CCA.2016.7587843 PDF
- Navarro-Tapia, D., Marcos, A., Bennani, S., Roux, C., “Structured H-infinity Control Based on Classical Control Parameters for the VEGA Launch Vehicle,” IEEE Multi-Conference on Systems and Control (MSC 2016), Buenos Aires, Argentina, September 2016. DOI10.1109/CCA.2016.7587818 PDF
- Joffre, E., Zamaro, M., Silva, N., Marcos, A., Simplicio, P., Richardson, B., “Landing on Small Bodies Trajectory Design, Robust Nonlinear Guidance and Control ,” 27th AAS/AIAA Space Flight Mechanics Meeting, San Antonio (Texas), USA, February 2017 PDF
- Marcos, A., Sato, M., “Robust Model-Matching Controller Design Using Matlab hinfstruct Command,” The 4th Multi-Symposium on Control Systems (SICE-MSCS17), Okayama, Japan, March 2017 PDF
- Iannelli, A., Marcos, A., Lowenberg, M., “LCO amplitude tailoring based on Describing Functions and Singular Structured Value Analysis,” 4th CEAS Specialist Conference on Guidance, Navigation and Control (EuroGNC 2017), Warsaw, Poland, April 2017 PDF
- Simplício, P., Marcos, A., Joffre, E., Zamaro, M., Silva, N., “Parameterised Laws for Robust Guidance and Control of Planetary Landers,” 4th CEAS Specialist Conference on Guidance, Navigation and Control (EuroGNC 2017), Warsaw, Poland, April 2017 PDF
- Navarro-Tapia, D., Marcos, A., Bennani, S., Roux, C., “Structured H-infinity Control Design for the VEGA Launch Vehicle: Recovery of the Legacy Control Behaviour,” ESA Guidance, Navigation and Control Conference (ESAGNC 2017), Salzburg, Austria, May 2017 PDF
- Joffre, E., Zamaro, M., Silva, N., Marcos, A., Simplicio, P., Richardson, B., “Results of new guidance and control strategies for landing on small bodies,” ESA Guidance, Navigation and Control Conference (ESAGNC 2017), Salzburg, Austria, May 2017 PDF
- Iannelli, A., Marcos, A., Lowenberg, M., “Nonlinear flutter analysis with uncertainties based on Describing Function and Structured Singular Value with an IQC validation,” 7th European Conference for Aeronautics and Space Sciences (EUCASS 2017), Milan, Italy, July 2017 PDF
- Navarro-Tapia, D., Marcos, A., Bennani, S., Roux, C., “Structured H-infinity and Linear Parameter Varying control design for the VEGA Launch Vehicle,” 7th European Conference for Aeronautics and Space Sciences (EUCASS 2017), Milan, Italy, July 2017 PDF ** Recommended for publication in ACTA Astronautica **
- Simplício, P., Marcos, A., Joffre, E., Zamaro, M., Silva, N., “A Systematic Performance-Oriented Tuning for Space Exploration Descent & Landing Guidance,” 7th European Conference for Aeronautics and Space Sciences (EUCASS 2017), Milan, Italy, July 2017 PDF ** Recommended for publication in ACTA Astronautica **
- Iannelli, A., Simplício, P., Navarro-Tapia, D., Marcos, A., “LFT Modeling and m Analysis of the Aircraft Landing Benchmark,” 20th IFAC World Congress, Toulouse, France, July 2017. doi.org/10.1016/j.ifacol.2017.08.766 PDF
- Navarro-Tapia, D., Simplício, P., Iannelli, A., Marcos, A., “Robust Flare Control Design Using Structured H-infinity Synthesis: a Civilian Aircraft Landing Challenge,” 20th IFAC World Congress, Toulouse, France, July 2017. doi.org/10.1016/j.ifacol.2017.08.769
- Marcos, A., Sato, M., “Flight Testing of an Structured H-infinity Controller: An EU-Japan Collaborative Experience,” 1st IEEE Conference on Control Technology and Applications (2017 CCTA), Hawai'i, US, August 2017 PDF
- Marcos, A., “Revisiting the aircraft C* control law: a comparison between classical and structured H-infinity designs,” 1st IEEE Conference on Control Technology and Applications (2017 CCTA), Hawai'i, US, August 2017 PDF
- Iannelli, A., Marcos, A., Lowenberg, M., “Nonlinear stability and post-critical analysis of an uncertain plant with Describing Functions and Integral Quadratic Constraints," Conference on Decision and Control (CDC2017), Melbourne, AUS, December 2017, DOI:10.1109/CDC.2017.8263913 PDF
- Simplício, P., Marcos, A., Joffre, E., Zamaro, M., Silva, N., “Robust Control Compensation for Space Descent & Landing,” 17th annual European Control Conference, Limassol, Cyprus, June 2018 PDF ** Recommended for publication in European Journal of Control **
- Iannelli, A., Marcos, A., Lowenberg, M., “Estimating the region of attraction of uncertain systems with invariant sets,” ROCOND, Florianopolis, Brazil, September 2018, https://doi.org/10.1016/j.ifacol.2018.11.113 PDF
- Simplício, P., Navarro-Tapia, D., Iannelli, A., Marcos, A., “From Standard to Structured Robust Control Design: Application to Aircraft Automatic Glide-Slope Approach,” ROCOND, Florianopolis, Brazil, September 2018 PDF
- Navarro-Tapia, D., Marcos, A., Bennani, S., Roux, C., “Linear Parameter Varying Control Synthesis for the atmospheric phase VEGA launcher,” 2nd LPVS, Florianopolis, Brazil, September 2018 PDF *** FINALIST IFAC Young Author Prize ***
- Navarro-Tapia, D., Marcos, A., Bennani, S., Roux, C., “Structured H-infinity Control Design for the VEGA Launcher: Robust Control Design Augmentation,” International Astronautical Congress (IAC), Bremen, Germany, October 2018 PDF
- Navarro-Tapia, D., Marcos, A., Bennani, S., Roux, C., “Reconciling Full-Order LPV Design and Augmented Structured H-infinity via Internal Model Principle,” IEEE 7th International Conference on Systems and Control (ICSC), Valencia, Spain, October 2018 PDF
- Iannelli, A., Marcos, A., Lowenberg, M., “Algorithms for the estimation of the region of attraction with positively invariant sets,” IEEE 7th International Conference on Systems and Control (ICSC), Valencia, Spain, October 2018, DOI:10.1109/ICoSC.2018.8587774 PDF
- Iannelli, A., Seiler, P., Marcos, A., “Estimating the region of attraction of uncertain systems with Integral Quadratic Constraints,” Conference on Decision and Control (CDC2018), Miami-Beach, USA, December 2018, DOI:10.1109/CDC.2018.8619669 PDF
- Iannelli, A., Seiler, P., Marcos, A., “An equilibrium-independent region of attraction formulation for systems with uncertainty-dependent equilibria,” Conference on Decision and Control (CDC2018), Miami-Beach, December USA, 2018, DOI:10.1109/CDC.2018.8619153 PDF
- Luspay, T., Ossmann, D., Wuestenhagen, M., Teubl, D., Baár, T., Péni, T., Pusch, M., Kier, T., Waitman, S., Iannelli, A., Marcos, A., Vanek, B., “Flight control design for a highly flexible flutter demonstrator,” AIAA Science and Technology Forum (SciTech 2019), San Diego, USA, January 2019, https://doi.org/10.2514/6.2019-1817 PDF
- Navarro-Tapia, D., Marcos, A., Bennani, S., Roux, C., “Robust-Control-Based Design and Comparison of an Adaptive Controller for the VEGA Launcher,” AIAA Science and Technology Forum (SciTech 2019), San Diego, USA, January 2019 PDF
- Simplício, P., Marcos, A., Bennani, S., “A Reusable Launcher Benchmark with Advanced Recovery Guidance,” 5th CEAS EuroGNC, Milan, Italy, April 2019 PDF
- Iannelli, A., Lowenberg, M., Marcos, A., “An extension of the structured singular value to nonlinear systems with application to robust flutter analysis,” 5th CEAS EuroGNC, Milan, Italy, April 2019 PDF ** Recommended for publication in CEAS Aeronautical Journal**
- Iannelli, A., Marcos, A., Bombardieri, R., Cavallaro, R., “A symbolic LFT approach for robust flutter analysis of high-order models,” European Control Conference, Naples, Italy, June 2019, DOI:10.23919/ECC.2019.8796122 PDF ** Recommended for publication in European Journal of Control **
- Navarro-Tapia, D., Marcos, A., Bennani, S., Roux, C., “Performance and robustness trade-off capabilities for the VEGA launcher TVC system,” 8th European Conference for Aeronautics and Space Science (EUCASS 2019), Madrid, SP, July 2019. DOI: 10.13009/EUCASS2019-351 PDF
- Simplício, P., Marcos, A., Bennani, S., “New Control Functionalities for Launcher Load Relief in Ascent and Descent Flight,” 8th European Conference for Aeronautics and Space Science (EUCASS 2019), Madrid, SP, July 2019 DOI: 10.13009/EUCASS2019-275 PDF *** WINNER Best Student Paper Award ***
- Waitman, S., Marcos, A., “Active flutter suppression: non-structured and structured H-infinity design,” 21st IFAC Symposium on Automatic Control in Aerospace (ACA 2019), Cranfield, UK, August 2019, DOI:https://doi.org/10.1016/j.ifacol.2019.11.184 PDF
- Waitman, S., Marcos, A., Sato, M., “Design and Hardware-In-the-Loop validation of a Fault-Tolerant Y* flight control law,” 4th International Conference on Control and Fault-Tolerant Systems (SYSTOL19), Casablanca, Morocco, September 2019. PDF
- Takarics, B., Patartics, B., Luspay, T., Vanek, B., Roessler, C., Bartasevicius, J., Koberle, S., Hornung, M., Tubl, D., Pusch, M., Wuestenhagen, M., Kier, T., Looye, G., Bauer, P., Meddaikar Y., Waitman, S., Iannelli, A., Marcos, A., Vanek, B., “Active Flutter Mitigation Testing on the FLEXOP Demonstrator Aircraft,” AIAA Science and Technology Forum (SciTech 2020), Orlando, USA, January 2020
- Takase, R., Marcos, A., Sato, M., Suzuki, S., “Hardware-In-The-Loop Evaluation of a Robust C* Control Law on MuPAL-a Research Aircraft,” 21st IFAC World Congress, Berlin, Germany, July 2020
- Sato, M., Marcos, A., “Observer-based Robust H-infinity Fault-Tolerant Flight Control: a Design Example and Performance Assessment,” Conference on Decision and Control (CDC2020), Jeju Island, Republic of Korea, December 2020
- Ponche, A., Marcos, A., Ott, T., Schleicher, A., “Investigation of Multi-Body/Multi-Actuator Modeling Techniques for Applicability to Future Space Observation Missions,” 11th ESA GNC conference, June 2021
- Simplício, P., Marcos, A., Bennani, S., “Multi-physics Launcher Modelling for Aeroelastic Load Predictions and Faster Design Iterations,” 8th International Conference on Astrodynamics Tools and Techniques (ICATT), June 2021
- Ponche, A., Marcos, A., Ott, T., Geshnizjani, R., “Advanced Guidance Strategy for Multi-Body/Multi-Actuator Spacecraft Repointing Under Sun Avoidance Constraints,” EUCASS conference, Lille, France, June 2022
- Navarro-Tapia, D., Marcos, A., Joost, V. “Enhanced AOCS verification techniques for Euclid's high-pointing performance,” ROCOND, Kyoto, Japan, August 2022
- Marcos, A., "A Linear Parameter Varying Model of the Boeing 747-100/200 Longitudinal Motion", MS thesis. Department of Aerospace and Engineering Mechanics, University of Minnesota, USA, January, 2001. PDF errata_PDF
- Marcos, A., "Aircraft Applications of Fault Detection and Isolation Techniques", PhD Thesis, Department of Aerospace and Engineering Mechanics, University of Minnesota, USA, February, 2004. PDF
- Marcos, A., Balas G.J., "A Boeing 747-100/200 Aircraft Fault Tolerant and Fault Diagnosis Benchmark", Technical Report, Department of Aerospace and Engineering Mechanics, University of Minnesota, USA, June, 2003. PDF
- Navarro-Tapia, D., "Robust and Adaptive TVC Control Design Approaches for the VEGA Launcher", PhD Thesis, Department of Aerospace Engineering, University of Bristol, UK, June, 2019. PDF
- Iannelli, A., "Robust Linear and Nonlinear Modeling and Analysis Approaches for Uncertain Aeroelastic Systems", PhD Thesis, Department of Aerospace Engineering, University of Bristol, UK, June, 2019. PDF
- Simplício, P., "Guidance and Control Elements for Improved Access to Space: from Planetary Landers to Reusable Launchers", PhD Thesis, Department of Aerospace Engineering, University of Bristol, UK, November, 2019. PDF