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Enrico Cavallini
Enrico Cavallini
Italian Space Agency (ASI) - Scientific Research Unit
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Modeling and Numerical Simulation of Solid Rocket Motors Internal Ballistics
E Cavallini
Sapienza, University of Rome, 2010
682010
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
462021
Internal ballistics simulation of a NAWC tactical SRM
E Cavallini, B Favini, M Di Giacinto, F Serraglia
372011
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
352022
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
252019
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
242010
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
232022
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
212020
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
212009
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
192022
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
172008
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
162020
Covariance control for stochastic low-thrust trajectory optimization
B Benedikter, A Zavoli, Z Wang, S Pizzurro, E Cavallini
AIAA SCITECH 2022 Forum, 2474, 2022
152022
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
152011
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
132023
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
122022
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
102020
Pressure oscillations simulation in P80 SRM first stage VEGA launcher
V Ferretti, B Favini, E Cavallini, F Serraglia, M Di Giacinto
47th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, San Diego …, 2011
102011
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