Modeling and Numerical Simulation of Solid Rocket Motors Internal Ballistics E Cavallini Sapienza, University of Rome, 2010 | 68 | 2010 |
Convex approach to three-dimensional launch vehicle ascent trajectory optimization B Benedikter, A Zavoli, G Colasurdo, S Pizzurro, E Cavallini Journal of Guidance, Control, and Dynamics 44 (6), 1116-1131, 2021 | 52 | 2021 |
Sliding mode control for attitude maneuvers of Helianthus solar sail M Bassetto, L Niccolai, L Boni, G Mengali, AA Quarta, C Circi, S Pizzurro, ... Acta Astronautica 198, 100-110, 2022 | 40 | 2022 |
Internal ballistics simulation of a NAWC tactical SRM E Cavallini, B Favini, M Di Giacinto, F Serraglia | 38 | 2011 |
Convex optimization of launch vehicle ascent trajectory with heat-flux and splash-down constraints B Benedikter, A Zavoli, G Colasurdo, S Pizzurro, E Cavallini Journal of Spacecraft and Rockets 59 (3), 900-915, 2022 | 31 | 2022 |
Convex approach to covariance control with application to stochastic low-thrust trajectory optimization B Benedikter, A Zavoli, Z Wang, S Pizzurro, E Cavallini Journal of Guidance, Control, and Dynamics 45 (11), 2061-2075, 2022 | 28 | 2022 |
State of art and current challenges of the paraffin-based hybrid rocket technology G Leccese, E Cavallini, M Pizzarelli AIAA propulsion and energy 2019 forum, 4010, 2019 | 27 | 2019 |
Numerical Simulations of Acoustic Resonance of Solid Rocket Motor V Ferretti, B Favini, E Cavallini, F Serraglia, M Di Giacinto 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Nashville …, 2010 | 24 | 2010 |
Autonomous upper stage guidance using convex optimization and model predictive control B Benedikter, A Zavoli, G Colasurdo, S Pizzurro, E Cavallini ASCEND 2020, 4268, 2020 | 22 | 2020 |
SRM Internal Ballistic Numerical Simulation by SPINBALL Model E Cavallini, B Favini, M Di Giacinto, F Serraglia 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Denver …, 2009 | 21 | 2009 |
Structural response of Helianthus solar sail during attitude maneuvers L Boni, M Bassetto, L Niccolai, G Mengali, AA Quarta, C Circi, ... Aerospace Science and Technology 133, 108152, 2023 | 18 | 2023 |
Large-eddy simulation of vortex shedding and pressure oscillations in solid rocket motors M Bernardini, M Cimini, F Stella, E Cavallini, A Di Mascio, A Neri, ... AIAA journal 58 (12), 5191-5201, 2020 | 18 | 2020 |
Covariance control for stochastic low-thrust trajectory optimization B Benedikter, A Zavoli, Z Wang, S Pizzurro, E Cavallini AIAA scitech 2022 forum, 2474, 2022 | 17 | 2022 |
Internal Ballistics Simulation of NAWC Tactical Motors with SPINBALL Model E Cavallini, B Favini, M Di Giacinto, F Serraglia 46th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Nashville …, 2010 | 17 | 2010 |
An Ignition-to-Burn Out Analysis of Internal Ballistic in Solid Rocket Motors M Di Giacinto, B Favini, E Cavallini, F Serraglia Space Propulsion 2008 - International Symposium on Propulsion for Space …, 2008 | 17* | 2008 |
An Ignition-to-Burn Out Analysis of SRM Internal Ballistic and Performances B Favini, E Cavallini, M Di Giacinto, F Serraglia 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Hartford …, 2008 | 17 | 2008 |
Internal Ballistics Modeling of High Performance SRMs with Coupled Nozzle Erosion Characterization E Cavallini, D Bianchi, B Favini, M Di Giacinto, F Serraglia 47th AIAA Joint Propulsion Conference and Exhibit 31-July to 3-Aug 2011 in …, 2011 | 15 | 2011 |
Autonomous upper stage guidance with robust splash-down constraint B Benedikter, A Zavoli, G Colasurdo, S Pizzurro, E Cavallini arXiv preprint arXiv:2212.06518, 2022 | 12 | 2022 |
A computational tool for the design of hybrid rockets PM Zolla, MT Migliorino, D Bianchi, F Nasuti, RC Pellegrini, E Cavallini Aerotecnica Missili & Spazio 100 (3), 253-262, 2021 | 11* | 2021 |
Convex optimization of launch vehicle ascent trajectory with heat-flux and splash-down constraints B Benedikter, A Zavoli, G Colasurdo, S Pizzurro, E Cavallini arXiv preprint arXiv:2008.13239, 2020 | 10 | 2020 |