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Paul Acquatella
Paul Acquatella
Otros nombresPaul Acquatella B.
GNC Engineer, Aurora Technology B.V. for ESA - European Space Agency
Dirección de correo verificada de ext.esa.int
Título
Citado por
Citado por
Año
Robust Nonlinear Spacecraft Attitude Control using Incremental Nonlinear Dynamic Inversion.
P Acquatella, W Falkena, EJ van Kampen, QP Chu
AIAA Guidance, Navigation, and Control Conference, 4623, 2012
742012
Incremental backstepping for robust nonlinear flight control
P Acquatella, E van Kampen, QP Chu
Proceedings of the EuroGNC 2013, 2013
602013
Guidance command generation and nonlinear dynamic inversion control for reusable launch vehicles
P Acquatella, LE Briese, K Schnepper
Acta Astronautica 174, 334-346, 2020
212020
Focused research on RLV-technologies: the DLR project AKIRA
M Sippel, S Stappert, J Wilken, N Darkow, S Cain, S Krause, T Reimer, ...
202019
PI(D) tuning for flight control systems via incremental nonlinear dynamic inversion
P Acquatella, W van Ekeren, QP Chu
IFAC-PapersOnLine 50 (1), 8175-8180, 2017
182017
Multidisciplinary modeling and simulation framework for launch vehicle system dynamics and control
LE Briese, P Acquatella, K Schnepper
Acta Astronautica 170, 652-664, 2020
162020
Development of Automation & Robotics in Space Exploration
P Acquatella
4th International Planetary Probe Workshop (IPPW-4), Pasadena, CA, June 2006, 2006
152006
Advanced modeling and trajectory optimization framework for reusable launch vehicles
LE Briese, K Schnepper, P Acquatella
2018 IEEE Aerospace Conference, 1-18, 2018
142018
Launch vehicle multibody dynamics modeling framework for preliminary design studies
P Acquatella
6th International Conference on Astrodynamics Tools and Techniques (ICATT …, 2016
122016
Modelica stage separation dynamics modeling for End-to-End launch vehicle trajectory simulations
P Acquatella B, MJ Reiner
Proceedings of the 10th International Modelica Conference-Lund, Sweden-Mar …, 2014
102014
Robust nonlinear spacecraft attitude control: An incremental backstepping approach
P Acquatella
102011
Fast Slew Maneuvers for the High-Torque-Wheels BIROS Satellite
P Acquatella B
TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES 61 (2 …, 2018
7*2018
Agile spacecraft attitude control: An incremental nonlinear dynamic inversion approach
P Acquatella, QP Chu
IFAC-PapersOnLine 53 (2), 5709-5716, 2020
62020
Algebraic estimation and control of single-link flexible joint robots
M Assanimoghaddam, P Acquatella
2017 IEEE/RSJ International Conference on Intelligent Robots and Systems …, 2017
52017
Design of a Control Allocation Solution for the Winged Reusable Launch Vehicle ReFEx
JLR Redondo Gutierrez, D Seelbinder, J Robens, P Acquatella
AIAA Scitech 2022 Forum, 1842, 2022
32022
The Reusability Flight Experiment–ReFEx: From Design to Flight–Hardware
P Rickmers, W Bauer, S Stappert, M Sippel, JL Redondo Gutierrez, ...
Proceedings of the International Astronautical Congress, IAC, 2021
32021
Multi-Disciplinary Modeling Environment for Reusable Launch Vehicle Dynamics and Control System Design
LE Briese, K Schnepper, P Acquatella
8th European Conference for Aeronautics and Aerospace Sciences (EUCASS), 2019
32019
Design and Development of R2M2-A Multi-Physics Modeling Tool for Reusable Launch Vehicles
B Gäßler, LE Briese, P Acquatella B, P Simplício, S Bennani, M Casasco
12023
Variable-Mass Dynamics Implementation in Multi-Physics Environment for Reusable Launcher Simulations
B Gäßler, LE Briese, P Acquatella B, P Simplício, S Bennani, M Casasco
12022
A Sampled-Data Form of Incremental Nonlinear Dynamic Inversion for Spacecraft Attitude Control
P Acquatella, EJ Van Kampen, QP Chu
AIAA SciTech 2022 Forum, 0761, 2022
12022
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