Michèle Lavagna

Full Professor

Politecnico di Milano

Italy

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About

Michèle Lavagna is a Full Professor at Politecnico di Milano, Italy. Her research areas focus on spacecraft guidance and control, lunar navigation, and advanced image processing techniques for proximity operations. Recent articles include contributions to robust lunar navigation constellations, spacecraft relative pose estimation, and autonomous lunar navigation methods. She is also involved in the development of innovative strategies for propulsive landing and ice-mining lunar rovers.

Articles (19)

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2025

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2022

Collaborators (2)

Giuseppe Cataldo

National Aeronautics and Space Administration (NASA)

UNITED STATES

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Paolo Lunghi

Assistant Professor

Politecnico di Milano

ITALY

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Michèle Lavagna

Research Interests

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About

Articles (19)

Design and station-keeping strategies for robust lunar navigation constellations

Reinforced Model Predictive Guidance and Control for Spacecraft Proximity Operations

Robust and efficient single-CNN-based spacecraft relative pose estimation from monocular images

Propulsive landing of launchers’ first stages with Deep Reinforcement Learning

Optical Image Generation Through Digital Terrain Models for Autonomous Lunar Navigation

Robust Onboard Orbit Determination Through Error Kalman Filtering

Synthetic thermal image generation and processing for close proximity operations

Ice-Mining Lunar Rover using Americium-241 Radioisotope Power Systems

Spacecraft and Asteroid Thermal Image Generation for Proximity Navigation and Detection Scenarios

Redundant Space Manipulator Autonomous Guidance for In-Orbit Servicing via Deep Reinforcement Learning

Planetary Soil Simulant Characterisation: NU-LHT-2M Study Case to Support Oxygen Extraction Lab Tests with a Low-Temperature Carbothermal Process

Coupling of Advanced Guidance and Robust Control for the Descent and Precise Landing of Reusable Launchers

Cross-Spectral Navigation with Sensor Handover for Enhanced Proximity Operations with Uncooperative Space Objects

Development of a Controlled Dynamics Simulator for Reusable Launcher Descent and Precise Landing

Exploiting Lunar Navigation Constellation for GNC Enhancement in Landing Missions

Model predictive control for formation reconfiguration exploiting quasi-periodic tori in the cislunar environment

An Effective Sensor Architecture for Full-Attitude Determination in the HERMES Nano-Satellites

Implicit Extended Kalman Filter for Optical Terrain Relative Navigation Using Delayed Measurements

Fault Tolerant Attitude and Orbit Determination System for Small Satellite Platforms

Collaborators (2)

Giuseppe Cataldo

Paolo Lunghi

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