Orbit design for LUMIO: The lunar meteoroid impacts observer

AM Cipriano, DA Dei Tos, F Topputo - Frontiers in Astronomy and …, 2018 - frontiersin.org
The Lunar Meteoroid Impacts Observer, or LUMIO, is a space mission concept awarded
winner of ESA's SysNova Competition “Lunar CubeSats for Exploration,” and as such it is …

Mission Analysis for the EM-1 CubeSats EQUULEUS and OMOTENASHI

S Campagnola, J Hernando-Ayuso… - IEEE Aerospace and …, 2019 - ieeexplore.ieee.org
OMOTENASHE and EQUULEUS are two 6-U CubeSats by JAXA and The University of
Tokyo to be launched in 2019 onboard of NASA's Exploration Mission 1. This paper …

Convex optimization over sequential linear feedback policies with continuous-time chance constraints

K Oguri, M Ono, JW McMahon - 2019 IEEE 58th Conference on …, 2019 - ieeexplore.ieee.org
The present paper extends the classically studied chance-constrained optimal control to
incorporate continuous-time chance constraints. While the classical approaches provide risk …

Attitude control: A key factor during the design of low-thrust propulsion for CubeSats

G Quinsac, B Segret, C Koppel, B Mosser - Acta Astronautica, 2020 - Elsevier
Orbital capability is a decisive step forward for nanosatellites in general and CubeSats in
particular. Although trajectory maneuvers and their implementation have been thoroughly …

Lunar far side positioning enabled by a CubeSat system deployed in an Earth-Moon halo orbit

H Chen, J Liu, L Long, Z Xu, Y Meng… - Advances in Space …, 2019 - Elsevier
For explorations of the far side of the Moon, it is necessary to tackle the challenge of
navigation and communication as the far side is invisible to the Earth. This paper proposes a …

Genetic optimization for the orbit maintenance of libration point orbits with applications to EQUULEUS and LUMIO

DA Dei Tos, N Baresi - AIAA Scitech 2020 Forum, 2020 - arc.aiaa.org
Many Earth-Moon libration point orbits are being evaluated as candidates for future space
missions, ranging from lunar gateways and possibly inhabited assets in the vicinity of the …

[PDF][PDF] LUMIO: a cubesat at Earth-Moon L2

F Topputo, M Massari, J Biggs, P Di Lizia… - 4S …, 2018 - re.public.polimi.it
ABSTRACT The Lunar Meteoroid Impact Observer (LUMIO) is a CubeSat mission to
observe, quantify, and characterize the meteoroid impacts by detecting their flashes on the …

Trajectory design and analysis of the LUMIO CubeSat

C Giordano, C Buonagura, A Martinelli… - AIAA Scitech 2024 …, 2024 - arc.aiaa.org
Meteoroids constantly impact the Earth–Moon system, posing risks to space assets and
threatening the life on the Earth. By studying lunar surface impacts, detailed information …

[PDF][PDF] EQUULEUS mission analysis: design of the transfer phase

K Oshima, S Campagnola, CH Yam, Y Kayama… - … Symposium on Space …, 2017 - issfd.org
This paper highlights the design of the transfer phase of EQUULEUS (EQUilibriUm Lunar-
Earth point 6U Spacecraft), which aims to reach and stay at the Earth-Moon L2 libration point …

Minimizing eclipses via synodic resonant orbits with applications to EQUULEUS and MMX

T Chikazawa, N Baresi, S Campagnola, N Ozaki… - Acta Astronautica, 2021 - Elsevier
For deep-space missions that remain in the vicinity of a target body, solar eclipses might
become a source of major concern due to thermal and power constraints. This paper …