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 | 82 | 2012 |
Incremental Backstepping for Robust Nonlinear Flight Control P Acquatella, E van Kampen, QP Chu Proceedings of the EuroGNC 2013, 2013 | 63 | 2013 |
Guidance command generation and nonlinear dynamic inversion control for reusable launch vehicles P Acquatella, LE Briese, K Schnepper Acta Astronautica 174, 334-346, 2020 | 25 | 2020 |
Focused research on RLV-technologies: the DLR project AKIRA M Sippel, S Stappert, J Wilken, N Darkow, S Cain, S Krause, T Reimer, ... | 20 | 2019 |
Multidisciplinary modeling and simulation framework for launch vehicle system dynamics and control LE Briese, P Acquatella, K Schnepper Acta Astronautica 170, 652-664, 2020 | 18 | 2020 |
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 | 18 | 2017 |
Development of Automation & Robotics in Space Exploration P Acquatella 4th International Planetary Probe Workshop (IPPW-4), Pasadena, CA, June 2006, 2006 | 15 | 2006 |
Advanced modeling and trajectory optimization framework for reusable launch vehicles LE Briese, K Schnepper, P Acquatella 2018 IEEE Aerospace Conference, 1-18, 2018 | 14 | 2018 |
Launch vehicle multibody dynamics modeling framework for preliminary design studies P Acquatella 6th International Conference on Astrodynamics Tools and Techniques (ICATT …, 2016 | 12 | 2016 |
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 | 12 | 2014 |
Agile spacecraft attitude control: An incremental nonlinear dynamic inversion approach P Acquatella, QP Chu IFAC-PapersOnLine 53 (2), 5709-5716, 2020 | 11 | 2020 |
Robust Nonlinear Spacecraft Attitude Control: An Incremental Backstepping Approach P Acquatella Master thesis, Delft University of Technology (2011), Faculty of Aerospace …, 2011 | 10 | 2011 |
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 | 8* | 2018 |
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 | 5 | 2017 |
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 | 4 | 2022 |
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 | 4 | 2022 |
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 | 4 | 2021 |
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 | 3 | 2019 |
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 | 2 | 2023 |
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 | 1 | 2022 |