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Andrea Colagrossi

Researcher at Polytechnic University of Milan

Publications -  24
Citations -  260

Andrea Colagrossi is an academic researcher from Polytechnic University of Milan. The author has contributed to research in topics: Rendezvous & Orbit (dynamics). The author has an hindex of 8, co-authored 24 publications receiving 152 citations.

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Proceedings ArticleDOI

The HERMES-technologic and scientific pathfinder

Fabrizio Fiore, +100 more
- 13 Dec 2020 - 
TL;DR: HERMES-TP/SP is a constellation of six 3U nano-satellites hosting simple but innovative X-ray detectors for the monitoring of Cosmic High Energy transients such as Gamma Ray Bursts and the electromagnetic counterparts of Gravitational Wave Events, and for the determination of their position.
Proceedings ArticleDOI

The scientific payload on-board the HERMES-TP and HERMES-SP CubeSat missions

Y. Evangelista, +102 more
- 14 Dec 2020 - 
TL;DR: HERMES (High Energy Rapid Modular Ensemble of Satellites) is a space-baring mission based on a LEO constellation of nano-satellites as mentioned in this paper.
Journal ArticleDOI

Preliminary results on the dynamics of large and flexible space structures in Halo orbits

TL;DR: In this article, a case study for a large and flexible space structure in Halo orbits around one of the Earth-Moon collinear Lagrangian points, L1 or L2, is discussed to point out some relevant outcomes for the potential implementation of such a mission.
Journal ArticleDOI

Guidance, navigation and control for 6DOF rendezvous in Cislunar multi-body environment

TL;DR: A guidance, navigation and control (GNC) framework for 6 degrees of freedom (6DOF) coupled Cislunar rendezvous and docking and a closed-loop GNC that encompasses coupled translational-rotational dynamics are proposed.
Journal ArticleDOI

Dynamical analysis of rendezvous and docking with very large space infrastructures in non-Keplerian orbits

TL;DR: The study addresses the dynamics during rendezvous and docking operations with a very large space infrastructure in an EML2 Halo orbit and takes into account the coupling effects between the orbital and the attitude motion in a circular restricted three-body problem environment.