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Pedro Simplicio
Pedro Simplicio
GNC Engineer, European Space Agency
Verified email at esa.int - Homepage
Title
Cited by
Cited by
Year
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
1692013
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
482016
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
452019
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
412020
Helicopter nonlinear flight control using incremental nonlinear dynamic inversion
PVM Simplício
Delft University of Technology, 2011
33*2011
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
302019
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
252017
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
242018
Trajectory design and guidance for landing on Phobos
E Joffre, M Zamaro, N Silva, A Marcos, P Simplício
Acta Astronautica 151, 389-400, 2018
162018
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
142017
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
112019
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
102021
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
102018
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
92017
Guidance and Control Elements for Improved Access to Space
P Simplicio
Ph. D. Thesis, Univ. of Bristol, Bristol, England, UK, 2019
82019
Landing on small bodies trajectory design, robust nonlinear guidance and control
E Joffre, M Zamaro, N Silva, A Marcos, P Simplício, B Richardson
The 27th AAS/AIAA Spacefilght Mechanics Meeting, San Antonio, TX, 2017
72017
Launcher flight control design using robust wind disturbance observation
P Simplício, A Marcos, S Bennani
Acta Astronautica 186, 303-318, 2021
62021
From standard to structured robust control design: application to aircraft automatic glide-slope approach
P Simplício, D Navarro-Tapia, A Iannelli, A Marcos
IFAC-PapersOnLine 51 (25), 140-145, 2018
62018
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
5*2020
A reusable launcher benchmark with advanced recovery guidance
P Simplicio, A Marcos, S Bennani
5th CEAS Conference on Guidance, Navigation & Control, 2019
52019
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Articles 1–20