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Reusable Launch Vehicles Re-Entry: Preliminary Architecture Towards Optimal Guidance and Control 1-gen-2021 De Oliveira, A. M. A.Lavagna, M.
Mission Analysis, GNC and ATD for Reusable Launch Vehicles within ASCenSIon: Multi-Orbit Multi-Payload Injection, Re-Entry and Safe Disposal 1-gen-2021 Alforja Ruiz, I.De Oliveira, A.Guadagnini, J.Lavagna, M. +
Reusable launchers re-entry controlled dynamics simulator 1-gen-2022 De Oliveira, A. M. A.Lavagna, M.
Assessment of Reusable Launch Vehicles Re-Entry Dynamics Control Effectiveness with Enhanced Aerodynamics Modelling 1-gen-2022 De Oliveira, A. M. A.Lavagna, M.
Advanced and Robust Guidance & Control System for the Recovery of Reusable Launchers 1-gen-2023 De Oliveira, A. M. A.Lavagna, M.
Robust Control Design via Structured H-Infinity for the Atmospheric Re-Entry of Reusable Launchers 1-gen-2023 De Oliveira, A. M. A.Lavagna, M.
Development of a Controlled Dynamics Simulator for Reusable Launcher Descent and Precise Landing 1-gen-2023 De Oliveira, AliceLavagna, Michèle
Advanced Guidance Design via Successive Convex Optimization for the 6-DoF Atmospheric Re-entry of Reusable Launchers 1-gen-2023 De Oliveira, A. M. A.Lavagna, M.
Coupling of Advanced Guidance and Robust Control for the Descent and Precise Landing of Reusable Launchers 1-gen-2024 De Oliveira, AliceLavagna, Michèle
Mostrati risultati da 1 a 9 di 9
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