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Matteo Ceriotti

Senior Lecturer in Space Systems Engineering

University of Glasgow

United Kingdom

Research Interests

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Articles (19)

Collaborators (3)

Robert Gordon

University of Glasgow

UNITED KINGDOM

Gilles BAILET

University of Glasgow

UNITED KINGDOM

Iain Moore

University of Glasgow

UNITED KINGDOM

ApplyKite TwinLearns as you apply

Make your next move.

Prepare your application

Review drafts before you send them.

Matteo Ceriotti

Research Interests

Make your next move.

Explore related searches

Articles (19)

Collaborators (3)

Robert Gordon

Gilles BAILET

Iain Moore

Make your next move.

Matteo Ceriotti

Research Interests

Make your next move.

Explore related searches

Articles (19)

Artificial neural network fine-tuning to increase accuracy of low-thrust space trajectory cost approximators

Guiding asteroids to form an artificial binary system using continuous control acceleration

Solar sail cooperative constellation control in displaced asteroid orbits

Displaced Solar Sail Orbits Around Asteroids with Free Angular Velocity

Transfer Learning for Sample-Efficient Training of Space Trajectory Cost Approximators

Corrigendum to “Analytical low-jerk reorientation maneuvers for multi-body spacecraft structures” [Acta Astronaut. 178 (2021) 1–14]

Broyden’s Method for Faster Inverse Simulation

Effects of model fidelity and uncertainty on a model-based attitude controller for satellites with flexible appendages

The capture of small near-Earth asteroids in a bound binary pair in Earth's orbit

Station-keeping for a solar sail during lander/probe deployment using feedback control

Low-Thrust, Multiple-Near-Earth-Asteroid Mission Design with Sample Return to Earth Using Machine Learning

A multiple-vehicle strategy for near-Earth asteroid capture

Design of multiple space debris removal missions using machine learning

Artificial Neural Networks for Multiple NEA Rendezvous Missions with Continuous Thrust

Comparison of material sources and customer locations for commercial space resource utilization

Asteroid Deflection by Leveraging Rotational Self-Energy

A simple control law for reducing the effective characteristic acceleration of a solar sail

End-to-end trajectory design for a solar-sail-only pole-sitter at Venus, Earth, and Mars

Sailing at the brink – The no-limits of near-/now-term-technology solar sails and SEP spacecraft in (multiple) NEO rendezvous

Collaborators (3)

Robert Gordon

Gilles BAILET

Iain Moore

Make your next move.