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Active space debris removal by a hybrid propulsion module

Acta astronautica, 2013-10, Vol.91, p.20-33

2013

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Multi-criteria design of continuous global coverage Walker and Street-of-Coverage constellations through property assessment

Acta astronautica, 2021-11, Vol.188, p.151-170

2021

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SD2 – How To Sample A Comet

Space science reviews, 2007-02, Vol.128 (1-4), p.281-299

2007

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Transfers to distant periodic orbits around the Moon via their invariant manifolds

Acta astronautica, 2012-10, Vol.79, p.20-32

2012

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Alta Scuola Politecnica: an ongoing experiment in the multidisciplinary education of top students towards innovation in engineering, architecture and design

European journal of engineering education, 2010-12, Vol.35 (6), p.627-643

2010

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Planning and implementation of the on-comet operations of the instrument SD2 onboard the lander Philae of Rosetta mission

Acta astronautica, 2016-08, Vol.125, p.183-195

2016

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Low-thrust planar transfer for co-planar low Earth orbit satellites considering self-induced collision avoidance

Aerospace science and technology, 2020-11, Vol.106, p.106198, Article 106198

2020

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High order optimal control of space trajectories with uncertain boundary conditions

Acta astronautica, 2014-01, Vol.93, p.217-229

2014

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High order optimal feedback control of space trajectories with bounded control

Acta astronautica, 2014-01, Vol.94 (1), p.383-394

2014

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The Value of Peer-Evaluation for the Improvement of Quality of the Aerospace Higher Education Across Europe

Aerotecnica, missili e spazio, 2017-04, Vol.96 (2), p.104-109

2017

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Earth‐to‐Moon Low Energy Transfers Targeting L 1 Hyperbolic Transit Orbits

Annals of the New York Academy of Sciences, 2005-12, Vol.1065 (1), p.55-76

2005

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Lessons Learned from the SD2 Operations on the Comet 67/P

Aerotecnica, missili e spazio, 2017-07, Vol.96 (3), p.148-153

2017

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On-Board Telemetry Monitoring via Support Vector Machine with Application to Philae Solar Generator

Aerotecnica, missili e spazio, 2018-10, Vol.97 (4), p.183-188

2018

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Simulation of Low-Intensity, Low-Temperature Solar Arrays with Software and Hardware Tools

Aerotecnica, missili e spazio, 2013-07, Vol.92 (3-4), p.94-100

2013

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Control of formation flight via extremum seeking

Proceedings of the 2002 American Control Conference (IEEE Cat. No.CH37301), 2002, Vol.4, p.2848-2853 vol.4

2002

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Attitude Dynamics of ESMO Satellite: Mass Expulsion Torques and Propellant Slosh Model

Aerotecnica, missili e spazio, 2013, Vol.92 (1-2), p.17-26

2013

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Philae Attitude Determination through Nonlinear Optimal Identification of Solar Arrays Telemetry

Aerotecnica, missili e spazio, 2014-07, Vol.93 (3-4), p.68-74

2014

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Sliding mode control of a large flexible space structure

Control engineering practice, 2000-08, Vol.8 (8), p.861-871

2000

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Wavefront interferometric technique for accurate spacecraft relative attitude determination

Optical engineering, 2005-02, Vol.44 (2), p.25603

Magnani, Piergiovanni

2005

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Optimizing Low-Thrust and Gravity Assist Maneuvers to Design Interplanetary Trajectories

The Journal of the astronautical sciences, 2003-01, Vol.51 (1), p.13-35

2003

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Active Flutter Suppression Using Recurrent Neural Networks

Journal of guidance, control, and dynamics, 2000-11, Vol.23 (6), p.1030-1036

2000

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SD2 : How to sample a comet: ROSETTA: Mission to comet 67P/Churyumov-Gerasimenko

Space science reviews, 2007, Vol.128 (1-4), p.281-299

2007

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Inverse Dynamics of Aircraft via Reduced-Order Shooting Methods

Journal of guidance, control, and dynamics, 2002-11, Vol.25 (6), p.1158-1162

2002

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Multi-Pulse-Width Modulated Control of Linear Systems

Journal of guidance, control, and dynamics, 1998-01, Vol.21 (1), p.64-70

1998

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Comment on "New Design Method for Pulse-Width Modulation Control Systems via Digital Redesign"

Journal of guidance, control, and dynamics, 2000-03, Vol.23 (2), p.381-382

2000

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Active space debris removal by a hybrid propulsion module

Multi-criteria design of continuous global coverage Walker and Street-of-Coverage constellations through property assessment

SD2 – How To Sample A Comet

Transfers to distant periodic orbits around the Moon via their invariant manifolds

Alta Scuola Politecnica: an ongoing experiment in the multidisciplinary education of top students towards innovation in engineering, architecture and design

Planning and implementation of the on-comet operations of the instrument SD2 onboard the lander Philae of Rosetta mission

Low-thrust planar transfer for co-planar low Earth orbit satellites considering self-induced collision avoidance

High order optimal control of space trajectories with uncertain boundary conditions

High order optimal feedback control of space trajectories with bounded control

The Value of Peer-Evaluation for the Improvement of Quality of the Aerospace Higher Education Across Europe

Earth‐to‐Moon Low Energy Transfers Targeting L 1 Hyperbolic Transit Orbits

Lessons Learned from the SD2 Operations on the Comet 67/P

On-Board Telemetry Monitoring via Support Vector Machine with Application to Philae Solar Generator

Simulation of Low-Intensity, Low-Temperature Solar Arrays with Software and Hardware Tools

Control of formation flight via extremum seeking

Attitude Dynamics of ESMO Satellite: Mass Expulsion Torques and Propellant Slosh Model

Philae Attitude Determination through Nonlinear Optimal Identification of Solar Arrays Telemetry

Sliding mode control of a large flexible space structure

Wavefront interferometric technique for accurate spacecraft relative attitude determination

Optimizing Low-Thrust and Gravity Assist Maneuvers to Design Interplanetary Trajectories

Active Flutter Suppression Using Recurrent Neural Networks

SD2 : How to sample a comet: ROSETTA: Mission to comet 67P/Churyumov-Gerasimenko

Inverse Dynamics of Aircraft via Reduced-Order Shooting Methods

Multi-Pulse-Width Modulated Control of Linear Systems

Comment on "New Design Method for Pulse-Width Modulation Control Systems via Digital Redesign"

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