TEOFILATTO, Paolo
TEOFILATTO, Paolo
SCUOLA DI INGEGNERIA AEROSPAZIALE
"On the Instability Induced by the Lunar Plane Motion on Earth Satellite Orbital Plane"
1994 Teofilatto, Paolo; Ulivieri, Carlo; Agneni, Alessandro
A control strategy for coordinated station keeping
1992 S., Carlini; M., Ceccarelli; Graziani, Filippo; Teofilatto, Paolo
A CONTROL SYSTEM FOR A SMALL SCALE ROCKET
2005 Luzzati, P.; Teofilatto, Paolo
A fast guidance algorithm for an autonomous navigation system
1997 Teofilatto, Paolo; E., De Pasquale
A magnetometer-only attitude determination strategy for small satellites: design of the algorithm and hardware-in-the-loop testing
2020 Carletta, Stefano; Teofilatto, Paolo; Farissi, Mohamed Salim
A measure for type II superstring
1990 M., Martellini; Teofilatto, Paolo
A nadir-pointing magnetic atitude control system for Tigrisat nanosatellite
2013 Teofilatto, Paolo; P., Testani; Celani, Fabio; Nascetti, Augusto; M., Truglio
A natural graded Lie algebra sheaf over variable Riemann surfaces
1991 Teofilatto, Paolo
A neural network based adaptive control for AOCS
1994 Santoni, Fabio; Teofilatto, Paolo; Graziani, Filippo
A new indirect measurement method of the electron temperature for the Proto-sphera's pinch plasma
2023 Iannarelli, D.; Napoli, F.; Alladio, F.; Apruzzese, G.; Bombarda, F.; Buratti, P.; Delfini, J.; De Ninno, A.; Filippi, F.; Fiorucci, D.; Ingenito, A.; Mannori, S.; Micozzi, P.; Teofilatto, P.
A New Neighboring Optimal Guidance Algorithm for Space Trajectories
2014 Pontani, Mauro; G., Cecchetti; Teofilatto, Paolo
A non linear adaptive algorithm for last stage launcher control
1999 Teofilatto, Paolo; E., DE PASQUALE
A paired Weil-Petersson inner product
1991 Teofilatto, Paolo
A paper and pencil method of evaluating trajectories of space launchers
2017 Teofilatto, P.
A proposal for passive stabilization of a satellite in eccentric orbit
1994 Teofilatto, Paolo; Graziani, Filippo
A prospective trajectory reconstruction system for a rocket model
2008 Teofilatto, Paolo; Ferroni, V; Agostinelli, M.
A ready to launch system by EFA carried small rocket
2005 Teofilatto, Paolo; Cesolari, P.
A semi-analytical evaluation of launcher performances
2001 E., DI SOTTO; Teofilatto, Paolo
A small scale low cost technology demonstrator of a reusable launch vehicle
2005 Chiesa, S.; Grassi, M.; Russo, G.; Teofilatto, Paolo
A strategy to find Weak Stability Boundary Lunar transfers
2000 Circi, Christian; Graziani, Filippo; M., Porfilio; Teofilatto, Paolo; M., Bello Mora; M., Hechler