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INNOCENTI, MARIO Statistiche

INNOCENTI, MARIO  

DIPARTIMENTO DI INGEGNERIA CIVILE E INDUSTRIALE  

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Titolo Data di pubblicazione Autore(i) File
Optimal time-fixed impulsive non-Keplerian orbit to orbit transfer algorithm based on primer vector theory 1-gen-2023 Bucchioni, Giordana; Gemignani, Gabriele; Lombardi, Francesco; Bellome, Andrea; Pedro Fernandes Leitão, João; Lizy-Destrez, Stèphanie; Innocenti, Mario
PRIMER VECTOR BASED OPTIMAL GUIDANCE FOR ORBITAL TRANSFERS IN CISLUNAR ENVIRONMENT 1-gen-2023 Gemignani, Gabriele; Bucchioni, Giordana; Lizy-Destrez, Stèphanie; Innocenti, Mario
Closed Loop Guidance during Close Range Rendezvous in a Three Body Problem 1-gen-2022 Galullo, M.; Bucchioni, G.; Franzini, G.; Innocenti, M.
Dynamics and control analysis during rendezvous in non-Keplerian Earth - Moon orbits 1-gen-2022 Innocenti, Mario; Bucchioni, Giordana; Franzini, Giovanni; Galullo, Michele; D'Onofrio, Fabio; Cropp, Alexander; Casasco, Massimo
Earth to Moon L2 NRHO Transfer using a Cycler Approach in the Restricted Three Body Problem 1-gen-2022 Donatini, Tommaso; D’Onofrio†, Fabio; Bucchioni‡, Giordana; Innocenti, Mario
Failure Mitigation during Rendezvous in Cislunar Orbit 1-gen-2022 D'Onofrio, F.; Innocenti, M.; Bucchioni, G.
Fully Safe Rendezvous Strategy in Cis-Lunar Space: Passive and Active Collision Avoidance 1-gen-2022 Bucchioni, Giordana; De Benedetti, Matteo; D'Onofrio, Fabio; Innocenti, Mario
Optimal Time-Fixed Impulsive non-Keplerian Orbit to Orbit Transfer 1-gen-2022 Bucchioni, Giordana; Lombardi, Francesco; Bellome, Andrea; Fernandes Leitao, Joao-Pedro; Innocenti, Mario; Lizy-Destrez, Stèphanie
An Adjoint-Based Method for Continuous Thrust Relative Maneuver Computation in the Restricted Three-Body Problem 1-gen-2021 Franzini, G.; Innocenti, M.; Casasco, M.
Bearings-only Guidance for Rendezvous in a Cis-lunar NRHO 1-gen-2021 D'Onofrio, F.; Bucchioni, G.; Innocenti, M.
Bearings-Only Guidance in Cis-Lunar Rendezvous 1-gen-2021 D’Onofrio, F.; Bucchioni, G.; Innocenti, M.
CLOSED-LOOP NEURAL CONTROL FOR THE FINAL PHASE OF A CISLUNAR RENDEZVOUS 1-gen-2021 Tofanelli, G; Bucchioni, G; Innocenti, M.
DESIGN OF THE PHASING TRAJECTORY FROM A LOW LUNAR ORBIT TO NEAR RECTILINEAR HALO ORBIT 1-gen-2021 Bucchioni, G.; Innocenti, M.
Design, Analysis and Selection of Haptic Inceptor Configurations for Tilt-Rotor Application * 1-gen-2021 Pollini, Lorenzo; Cavaliere, Chiara; Innocenti, Mario; Bulthoff, Heinrich; Teufel, Harald; Mozzillo, Luca; Benincasa, Marcello; Maiorca, Enrico; Scarabattoli, Davide; Ferri, Fabio; Blasio, Danilo di
Ephemeris validation of Rendezvous Guidance in Lunar NRHO 1-gen-2021 Bucchioni, G.; Innocenti, M.
Phasing Maneuver Analysis from a Low Lunar Orbit to a Near Rectilinear Halo Orbit 1-gen-2021 Bucchioni, G.; Innocenti, M.
Rendezvous in Cis-lunar Space Near Rectilinear Halo Orbit: Dynamics and Control Issues 1-gen-2021 Bucchioni, G.; Innocenti, M.
ROSSONERO: NEW FEATURES IN THE SIMULATION TOOL FOR REALISTIC RENDEZVOUS MISSION DESIGN IN THE RESTRICTED THREE-BODY PROBLEM 1-gen-2021 Bucchioni, G.; D'Onofrio, F; Innocenti, M.
A Fuzzy Guidance System for Rendezvous and Pursuit of Moving Targets 1-gen-2020 Alibani, M.; Innocenti, M.; Pollini, L.
Design of Phasing Trajectories From a Low Lunar Orbit To a Near Rectilinear Halo Orbit 1-gen-2020 Bucchioni, G.; Innocenti, M.