Paolo Teofilatto | Ricerc@Sapienza

Pubblicazioni

Titolo	Pubblicato in	Anno
An accurate modeling and performance of multistage launch vehicles for microsatellites via a firekwokk algorithm	Advances in Mathematics Research	2017
A paper and pencil method of evaluating trajectories of space launchers	Proceedings of the International Astronautical Conference	2017
Polyhedral representation of invariant manifolds applied to orbit transfers in the Earth-Moon system	ACTA ASTRONAUTICA	2016
Accurate modeling and near optimal ascent trajectory of microsatellite launch vehicles via firework algorithm	Proceedings of the International Astronautical Congress, IAC	2016
High gain S-band patch antenna system for Earth observation cubesat satellites	IEEE ANTENNAS AND WIRELESS PROPAGATION LETTERS	2015
Swirling combustor energy converter: H2/air simulations of separated chambers	ENERGIES	2015
IAC-15-B4.4.8 Earth observation with tigrisat: Structural and mission design	Proceedings of 66th International Astronautical Congress IAC-15PROCEEDINGS OF THE INTERNATIONAL ASTRONAUTICAL CONGRESS	2015
Variable-time-domain neighboring optimal guidance applied to space trajectories	ACTA ASTRONAUTICA	2015
Variable-time-domain neighboring optimal guidance, part 2: Application to lunar descent and soft landing	JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS	2015
Invariant manifold dynamics VIA polyhedral representation	Proceedings of the International Astronautical Congress, IAC	2015
Neighboring optimal guidance for soft lunar landing	Advances in the Astronautical Sciences	2015
Variable-time-domain neighboring optimal guidance, part 1: Algorithm structure	JOURNAL OF OPTIMIZATION THEORY AND APPLICATIONS	2015