Combined chemical--electric propulsion design and hybrid trajectories for stand-alone deep-space CubeSats
KV Mani - 2020 - politesi.polimi.it
Interplanetary CubeSats enable universities and small-spacecraft consortia to pursue low-
cost, high-risk and high-gain Solar System exploration missions, especially Mars missions …
cost, high-risk and high-gain Solar System exploration missions, especially Mars missions …
[PDF][PDF] Systems Design of MARIO: Stand-alone 16U CubeSat from Earth to Mars
KV Mani, AS Casado, V Franzese… - 70th International …, 2019 - researchgate.net
Mars Atmospheric Radiation Imaging Orbiter (MARIO) is a 16U stand-alone CubeSat
mission that shall escape Earth, perform autonomous deep-space cruise, achieve ballistic …
mission that shall escape Earth, perform autonomous deep-space cruise, achieve ballistic …
CubeSat Technology Past and Present: Current State-of-the-Art Survey
BMM Bomani - 2021 - ntrs.nasa.gov
A cube satellite (CubeSat) is an evolving and emerging technology that gives a novice or
advanced researcher relatively affordable access to space research experiments and …
advanced researcher relatively affordable access to space research experiments and …
Low-thrust station-keeping on libration point orbits leveraging supervised learning
A Gallina - 2022 - politesi.polimi.it
Computationally efficient guidance is challenging for station-keeping applications in
nonlinear dynamical regions, where a potential onboard control method must satisfy mission …
nonlinear dynamical regions, where a potential onboard control method must satisfy mission …
[PDF][PDF] Modeling of Solar Array Drive Assembly (SADA) for LUMIO spacecraft
BF Nicola - 2020 - researchgate.net
The considered real system is the Lunar Meteoroid Impact Observer (LUMIO) spacecraft.
LUMIO is a CubeSat mission to a quasi-halo orbit at Earth–Moon L2 that shall observe …
LUMIO is a CubeSat mission to a quasi-halo orbit at Earth–Moon L2 that shall observe …
Libration point orbit station-keeping: control strategies for improved scientific mission time
L Guerreschi - 2019 - politesi.polimi.it
The scientific interest in the exploitation of Lagrangian points orbits has increased in the last
decades. The requirement of precise station-keeping for the unstable motion of Halo orbits …
decades. The requirement of precise station-keeping for the unstable motion of Halo orbits …
Discrete active disturbance rejection control for halo orbit station-keeping
W Khoury - 2019 - politesi.polimi.it
This thesis addresses the problem of deep-space station-keeping of an L2 elliptic halo orbit
in the Earth-Moon system. A robust control approach is developed to guarantee closed-loop …
in the Earth-Moon system. A robust control approach is developed to guarantee closed-loop …