Giovanni Mengali

Professor

University of Pisa

Italy

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Giovanni Mengali is a Professor at the Università di Pisa, Italy. His research focuses on advanced trajectory design and control strategies for solar sails in uncertain environments, as well as the development of nonlinear control methods for spacecraft. Recent publications include work on robust NMPC strategies, deep reinforcement learning applications, and performance optimization in space missions.

Giovanni Mengali

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Articles (26)

Robust NMPC strategy for solar sail trajectory control in uncertain environments

Solar Sail Trajectory Design With Pulsed Radial Thrust

Robust solar sail trajectories using proximal policy optimization

Solar Sail Transfers under Uncertainties: A Deep Reinforcement Learning Approach

Electric Sail Test Cube–Lunar Nanospacecraft, ESTCube-LuNa: Solar Wind Propulsion Demonstration Mission Concept

Drag sail attitude tracking via nonlinear control

Trajectory Approximation of a Low-Performance E-Sail with Fixed Orientation

Solar Sail Optimal Performance in Heliocentric Nodal Flyby Missions

FEM-based eigenstructure recovery of a space truss with active members

Optimal Trajectories of Diffractive Sail to Highly Inclined Heliocentric Orbits

Optimal guidance laws for diffractive solar sails with Littrow transmission grating

Performance Estimate of a Spin-Stabilized Drag Sail for Spacecraft Deorbiting

Analytical Tool for Thrust Vector Description of a Web-Shaped E-Sail

Spacecraft Relative Motion Control Near an Asteroid With Uncertainties: A Lyapunov Redesign Approach

Decay time estimate for LEO spacecraft

Deterministic Trajectory Design and Attitude Maneuvers of Gradient-Index Solar Sail in Interplanetary Transfers

Circular Orbit Flip Trajectories Generated by E-Sail

Electric Sail Mission Expeditor, ESME: Software Architecture and Initial ESTCube Lunar Cubesat E-Sail Experiment Design

Solar Sail Orbit Raising with Electro-Optically Controlled Diffractive Film

Solar Sail Trajectories to Earth’s Trojan Asteroids

E-Sail Option for Plunging a Spacecraft into the Sun’s Atmosphere

Trajectory Analysis of a Zero-Pitch-Angle E-Sail with Homotopy Perturbation Technique

Optimal Interplanetary Transfer of Solar Wind Ion Focusing Thruster-Based Spacecraft

E-Sail Optimal Trajectories to Heliostationary Points

Along-Track Boundedness Condition for Spacecraft Relative Motion Around a Slowly Rotating Asteroid

Refined MagSail thrust model for preliminary mission design and trajectory optimization

Collaborators (5)

ALESSANDRO ANTONIO QUARTA

Nickolay Ivchenko

Marco Bassetto

Martin Tajmar

Andris Slavinskis

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