| 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 | 72 | 2012 |
| Incremental backstepping for robust nonlinear flight control P Acquatella, E van Kampen, QP Chu Proceedings of the EuroGNC 2013, 2013 | 60 | 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 | 21 | 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 |
| 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 |
| Multidisciplinary modeling and simulation framework for launch vehicle system dynamics and control LE Briese, P Acquatella, K Schnepper Acta Astronautica 170, 652-664, 2020 | 16 | 2020 |
| 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 | 13 | 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 |
| Robust nonlinear spacecraft attitude control: An incremental backstepping approach P Acquatella | 10 | 2011 |
| 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 | 9 | 2014 |
| 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 | 6 | 2020 |
| 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 |
| 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 | 3 | 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 | 3 | 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 |
| Multidisciplinary modeling and simulation framework for reusable launch vehicle system dynamics and control LE Briese, P Acquatella, K Schnepper 7th International Conference on Astrodynamics Tools and Techniques (ICATT) 11, 2018 | 1 | 2018 |
| Launcher Attitude Control based on Incremental Nonlinear Dynamic Inversion: A Feasibility Study Towards Fast and Robust Design Approaches P Simplício, P Acquatella, S Bennani arXiv preprint arXiv:2307.00372, 2023 | | 2023 |
| ReFEx: Reusability Flight Experiment-Design of an Exoatmospheric Control System J Robens, B Gäßler, P Acquatella B Aerospace Europe Conference 2023-10th EUCASS-9th CEAS, 2023 | | 2023 |
Q.P. ChuAssociate Professor of Aerospace Guidance, Navigation and Control, TU DelftGeverifieerd e-mailadres voor tudelft.nl
