G. Mingotti

发表

HIGH AREA-TO-MASS RATIO AND SMALL LENGTH-SCALE SPACECRAFT FORMATION FLYING APPLICATIONS

C. McInnes, G. Mingotti, 2013 .

Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun–Earth circular restricted three-body problem

C. McInnes, G. Mingotti, J. P. Sánchez, 2014 .

Low Energy, Low-Thrust Capture of Near Earth Objects in the Sun-Earth and Earth-Moon Restricted Three-Body Systems

C. McInnes, J. Sánchez, G. Mingotti, 2014 .

Intersecting invariant manifolds in spatial restricted three-body problems: Design and optimization of Earth-to-halo transfers in the Sun–Earth–Moon scenario

M. Dellnitz, G. Mingotti, Anna Zanzottera, 2012 .

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

F. Topputo, F. Bernelli-Zazzera, G. Mingotti, 2012 .

Attainable sets in space mission design : A method to define low-thrust, invariant manifold trajectories

F. Topputo, G. Mingotti, Franco Bernelli-Zazzara, 2012 .

Efficient invariant-manifold, low-thrust planar trajectories to the Moon

F. Topputo, F. Bernelli-Zazzera, G. Mingotti, 2012 .

Optimal low-thrust invariant manifold trajectories via attainable sets

F. Topputo, F. Bernelli-Zazzera, G. Mingotti, 2011 .

Earth–Mars transfers with ballistic escape and low-thrust capture

F. Topputo, F. Bernelli-Zazzera, G. Mingotti, 2011 .

Ways to the Moon : A survey

F. Topputo, G. Mingotti, 2011 .

Invariant-Manifold, Low-Thrust Transfers to Low Mars Orbits

F. Topputo, G. Mingotti, F. B. Zazzera, 2010 .

Mixed low-thrust invariant-manifold transfers to distant prograde orbits around Mars

P. Gurfil, G. Mingotti, 2010 .

Numerical Methods to Design Low-Energy, Low-Thrust Sun-Perturbed Transfers to the Moon

F. Topputo, G. Mingotti, F. B. Zazzera, 2009 .

Low-energy, low-thrust transfers to the Moon

F. Topputo, F. Bernelli-Zazzera, G. Mingotti, 2009 .

Optimal solar sail transfers between halo orbits of different sun-planet systems

Colin R. McInnes, Giorgio Mingotti, Jeannette Heiligers, 2015 .

Combined Optimal Low‐Thrust and Stable‐Manifold Trajectories to the Earth‐Moon Halo Orbits

Francesco Topputo, Franco Bernelli-Zazzera, Giorgio Mingotti, 2007 .

Autonomous satellite constellation for enhanced Earth coverage using coupled selection equations

C. McInnes, C. Colombo, G. Mingotti, 2013 .

Combined low-thrust propulsion and invariant manifold trajectories to capture NEOs in the Sun–Earth circular restricted three-body problem

C. McInnes, G. Mingotti, J. P. Sánchez, 2014, Celestial Mechanics and Dynamical Astronomy.

Heiligers, Jeannette and Mingotti, Giorgio and McInnes, Colin (2015) Optimal solar sail transfers between halo orbits of different sun-planet

C. McInnes, G. Mingotti, J. Heiligers, 2018 .

Optimal solar sail interplanetary heteroclinic transfers for novel space applications

Giorgio Mingotti, Jeannette Heiligers, Colin R. McInnes, 2014 .

First-guess generation of solar sail interplanetary heteroclinic connections

Colin R. McInnes, Giorgio Mingotti, Jeannette Heiligers, 2014 .

OPTIMISATION OF SOLAR SAIL INTERPLANETARY

C. McInnes, G. Mingotti, J. Heiligers, 2014 .

A Method to Design Efficient Low-Energy, Low-Thrust Transfers to the Moon

Francesco Topputo, Franco Bernelli-Zazzera, Giorgio Mingotti, 2011 .

Mixed Low-Thrust and Invariant-Manifold Transfers to Unstable Distant Prograde Orbits around Mars

P. Gurfil, G. Mingotti, 2010 .

Multiple-spacecraft transfers to Sun-Earth distant retrograde orbits for asteroid detection missions

C. McInnes, C. Colombo, G. Mingotti, 2014 .

Self-organising satellite constellation in geostationary earth orbit

C. McInnes, C. Colombo, G. Mingotti, 2015, IEEE Transactions on Aerospace and Electronic Systems.