Mauro Pontani

Sapienza University of Rome

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Articles (20)

Collaborators (4)

Elena Fantino

UNITED ARAB EMIRATES

paolo gasbarri

Università degli Studi di Roma La Sapienza

Simone Battistini

Head of Simulation & Modeling

Direnc Atmaca

Delft University of Technology

Mauro Pontani

Research Interests

Explore related searches

Contact this professor

Articles (20)

Collaborators (4)

Elena Fantino

paolo gasbarri

Simone Battistini

Direnc Atmaca

How do I reach out?

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Mauro Pontani

Research Interests

Explore related searches

Contact this professor

Articles (20)

Autonomous guidance and control for rendezvous and mating with gateway with collision avoidance maneuvering

Guidance strategies to deploy a Lunar Navigation Constellation from Gateway

Optimal low-thrust orbit transfers connecting Gateway with Earth and Moon

Minimum-Fuel Trajectories and Near-Optimal Explicit Guidance for Pinpoint Landing from Low Lunar Orbit

Nonlinear Orbit Acquisition and Maintenance of a Lunar Navigation Constellation Using Low-Thrust Propulsion

Berthing proximity maneuvers and trajectory planning of a space manipulator via Kane’s formulation

Near-Optimal Feedback Guidance for Low-Thrust Earth Orbit Transfers

Optimization, guidance, and control of low-thrust transfers from the Lunar Gateway to low lunar orbit

Orbit Rendezvous Maneuvers in Cislunar Space via Nonlinear Hybrid Predictive Control

Multiple-arc optimization of low-thrust Earth–Moon orbit transfers leveraging implicit costate transformation

Nonlinear attitude maneuvering of a flexible spacecraft for space debris tracking and collision avoidance

Special Issue on Small Satellites Missions and Applications

Lunar descent and landing via two-phase explicit guidance and pulse-modulated reduced-attitude control

Orbit acquisition, rendezvous, and docking with a noncooperative capsule in a Mars sample return mission

Statistical Study of Uncontrolled Geostationary Satellites near an Unstable Equilibrium Point

Low-Thrust Lunar Capture Leveraging Nonlinear Orbit Control

Low-Thrust Transfer to Quasi-Synchronous Martian Elliptic Orbit via Nonlinear Feedback Control

Mars orbit injection via aerocapture and low-thrust nonlinear orbit control

Explicit Near-Optimal Guidance and Pulse-Modulated Control for Lunar Descent and Touchdown

Mars Constellation Design and Low-Thrust Deployment Using Nonlinear Orbit Control

Collaborators (4)

Elena Fantino

paolo gasbarri

Simone Battistini

Direnc Atmaca

How do I reach out?

Meet Kite AI