NUGNES, MARCO

NUGNES, MARCO  

DIPARTIMENTO DI SCIENZE E TECNOLOGIE AEROSPAZIALI  

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Risultati 1 - 17 di 17 (tempo di esecuzione: 0.026 secondi).
Titolo Data di pubblicazione Autori File
A New Analytical Method for Eclipse Entry/Exit Positions Determination Considering a Conical Shadow and an Oblate Earth Surface 1-gen-2022 Nugnes, M.Colombo, C.
A New Methodology for the Solution of the Stiffness Problem Applied to Low-Thrust Trajectory Optimisation in Terms of Orbital Elements Using Differential Dynamic Programming 1-gen-2022 Nugnes, M.Colombo, C.
A system engineering tool for the optimisation of a GNSS constellation design 1-gen-2018 Nugnes, M.Colombo, C. +
A system-level engineering approach for preliminary performance analysis and design of global navigation satellite system constellations 1-gen-2020 Nugnes M.Colombo C. +
A System-Level Engineering Approach to Define the Social Value Rating of Earth Remote Sensing Missions Through Sustainable Development Goals 1-gen-2020 Nugnes, M.Colombo, C. +
Analytical determination of eclipse entry and exit points considering a conical shadow and oblate Earth 1-gen-2023 Nugnes, MColombo, C
COMPASS: Control for orbit manoeuvring enhancing natural perturbations 1-gen-2019 Colombo C.Gaias G.Gkolias I.Gonzalo J.MIGUEL BANOS, NARCÍSTrisolini M.Frey S.Huang S.Menzio D.NUGNES, MARCORomano M.
Coverage Area Determination for Conical Fields of View Considering an Oblate Earth 1-gen-2019 Nugnes, MarcoColombo, Camilla +
Data Fusion and Machine Learning for Innovative GNSS Science Use Cases 1-gen-2021 Nugnes, M. +
Introduction to a Keplerian-Orbital-Element-Based Optimisation Approach Via Differential Dynamic Programming 1-gen-2019 Nugnes, M.Colombo, C.
Low Thrust Multiple Revolution Transfer Design Using Artificial Potential Guidance in the Phase Space 1-gen-2019 Borelli, G.Nugnes, M.Colombo, C.
Low-thrust Optimal Trajectories using Differential Dynamic - Programming enhancing the effects of Orbital Perturbations 1-gen-2021 Nugnes, M.
Low-thrust Trajectory Optimisation through Differential Dynamic Programming Method based on Keplerian Orbital Elements 1-gen-2019 Nugnes, M.Colombo, C.
Mission Analysis and Design for an Active Debris Removal Service for Large Constellations 1-gen-2021 Colombo, C.Huang, S.Borelli, G.Cavenago, F.Nugnes, M.Gonzalo Gòmez, J. L.Gaias, G.Massari, M. +
Multi-Revolution Low-Thrust Trajectory Optimisation Using Differential Dynamic Programming in Orbital Element Formulation 1-gen-2022 Nugnes, M.Colombo, C.
Preliminary Mission Analysis of Active Debris Removal Service for Large Constellations 1-gen-2020 Huang, S.Colombo, C.Gonzalo Gòmez, J. L.Nugnes, M. +
Social Benefits Assessment of Earth Observation Missions Through the SDG2030 1-gen-2021 Nugnes, M.Colombo, C. +