| An acceleration measurements-based approach for helicopter nonlinear flight control using incremental nonlinear dynamic inversion P Simplício, MD Pavel, E Van Kampen, QP Chu Control Engineering Practice 21 (8), 1065-1077, 2013 | 201 | 2013 |
| 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 | 56 | 2019 |
| 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 | 54 | 2020 |
| Structured singular-value analysis of the VEGA launcher in atmospheric flight P Simplício, S Bennani, A Marcos, C Roux, X Lefort Journal of Guidance, Control, and Dynamics 39 (6), 1342-1355, 2016 | 53 | 2016 |
| Helicopter nonlinear flight control using incremental nonlinear dynamic inversion PVM Simplício Delft University of Technology, 2011 | 36* | 2011 |
| 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 | 35 | 2018 |
| Legacy recovery and robust augmentation structured design for the VEGA launcher D Navarro‐Tapia, A Marcos, P Simplício, S Bennani, C Roux International Journal of Robust and Nonlinear Control 29 (11), 3363-3388, 2019 | 33 | 2019 |
| Robust flare control design using structured H∞ synthesis: A civilian aircraft landing challenge D Navarro-Tapia, P Simplicio, A Iannelli, A Marcos IFAC-PapersOnLine 50 (1), 3971-3976, 2017 | 28 | 2017 |
| New control functionalities for launcher load relief in ascent and descent flight P Simplício, A Marcos, S Bennani Proceedings of the 8th European Conference for Aeronautics and Aerospace …, 2019 | 16 | 2019 |
| Trajectory design and guidance for landing on Phobos E Joffre, M Zamaro, N Silva, A Marcos, P Simplício Acta Astronautica 151, 389-400, 2018 | 16 | 2018 |
| Combined control and navigation approach to the robotic capture of space vehicles Z Pavanello, F Branz, A Francesconi, A Cenedese, R Antonello, F Basana, ... INTERNATIONAL ASTRONAUTICAL CONGRESS: IAC PROCEEDINGS, 1-13, 2021 | 15 | 2021 |
| LFT modeling and μ analysis of the aircraft landing benchmark A Iannelli, P Simplício, D Navarro-Tapia, A Marcos IFAC-PapersOnLine 50 (1), 3965-3970, 2017 | 14 | 2017 |
| Guidance and Control Elements for Improved Access to Space P Simplicio Ph. D. Thesis, Univ. of Bristol, Bristol, England, UK, 2019 | 12 | 2019 |
| Launcher flight control design using robust wind disturbance observation P Simplício, A Marcos, S Bennani Acta Astronautica 186, 303-318, 2021 | 11 | 2021 |
| Synthesis and analysis of robust control compensators for Space descent & landing P Simplício, A Marcos, E Joffre, M Zamaro, N Silva International Journal of Robust and Nonlinear Control 28 (13), 3871-3892, 2018 | 10 | 2018 |
| Parameterised laws for robust guidance and control of planetary landers PVM Simplicio, A Marcos, E Joffre, M Zamaro, N Silva 4th CEAS Specialist Conference on Guidance, Navigation & Control (EURO GNC 2017), 2017 | 9 | 2017 |
| Landing on small bodies trajectory design, robust nonlinear guidance and control E Joffre, M Zamaro, N Silva, A Marcos, P Simplício, B Richardson 27th AAS/AIAA Space Flight Mechanics Meeting, 2017, 1425-1444, 2017 | 7 | 2017 |
| Physical modeling and simulation of electro-mechanical actuator-based TVC systems for reusable launch vehicles S Farì, D Seelbinder, S Theil, P Simplicio, S Bennani Acta Astronautica 214, 790-808, 2024 | 6 | 2024 |
| Robust control for launchers: VEGA study case A MARCOS, D Navarro-Tapia, P Simplício, S Bennani Journal of The Society of Instrument and Control Engineers 59 (3), 192-202, 2020 | 6* | 2020 |
| A reusable launcher benchmark with advanced recovery guidance P Simplicio, A Marcos, S Bennani 5th CEAS Conference on Guidance, Navigation & Control, 2019 | 6 | 2019 |
andres marcosUniversidad Carlos III de Madrid & Technology for Aerospace Control Ltd.ing.uc3m.es üzerinde doğrulanmış e-posta adresine sahip
