[HTML][HTML] Autonomous navigation for deep space small satellites: Scientific and technological advances

E Turan, S Speretta, E Gill - Acta Astronautica, 2022 - Elsevier
In recent years, there is a growing interest in small satellites for deep space exploration. The
current approach for planetary navigation is based on ground-based radiometric tracking. A …

EQUULEUS trajectory design

K Oguri, K Oshima, S Campagnola, K Kakihara… - The Journal of the …, 2020 - Springer
This paper presents the trajectory design for EQUilibriUm Lunar-Earth point 6U Spacecraft
(EQUULEUS), which aims to demonstrate orbit control capability of CubeSats in the cislunar …

Robust space trajectory design using belief optimal control

C Greco, S Campagnola, M Vasile - Journal of Guidance, Control, and …, 2022 - arc.aiaa.org
This paper presents a novel approach to the robust solution of optimal impulsive control
problems under aleatory and epistemic uncertainty. The novel approach uses belief Markov …

Environmental assessment in the prelaunch phase of Hayabusa2 for safety declaration of returned samples from the asteroid (162173) Ryugu: Background monitoring …

K Sakamoto, Y Takano, H Sawada, R Okazaki… - earth, planets and …, 2022 - Springer
We report ground-based environmental assessments performed during development of the
sampler system until the launch of the Hayabusa2 spacecraft. We conducted static …

Effective stability of quasi-satellite orbits in the spatial problem for phobos exploration

H Chen, E Canalias, D Hestroffer, X Hou - Journal of Guidance, Control …, 2020 - arc.aiaa.org
The generation of bounded trajectories complying with operational constraints in the
complex dynamic environment surrounding Phobos is not an easy task. The vicinity of …

Nano semihard moon lander: OMOTENASHI

T Hashimoto, T Yamada, M Otsuki… - IEEE Aerospace and …, 2019 - ieeexplore.ieee.org
The 6U CubeSat “OMOTENASHI,” which is due to be launched in 2020 by NASA's Space
Launch System, will be the world's smallest moon lander. Its main mission is to present the …

Construction of ballistic lunar transfers in the earth-moon-sun system

ST Scheuerle - 2021 - search.proquest.com
An increasing interest in lunar exploration calls for low-cost techniques of reaching the
Moon. Ballistic lunar transfers are long duration trajectories that leverage solar perturbations …

A single-launch deployment strategy for lunar constellations

S Carletta - Applied Sciences, 2023 - mdpi.com
Satellite constellations can provide communication and navigation services to support future
lunar missions, and are attracting growing interest from both the scientific community and …

Asteroid flyby cycler trajectory design using deep neural networks

N Ozaki, K Yanagida, T Chikazawa… - Journal of Guidance …, 2022 - arc.aiaa.org
Asteroid exploration has been attracting more attention in recent years. Nevertheless, we
have just visited tens of asteroids, whereas we have discovered more than 1 million bodies …

Flight model development and ground demonstration of water resistojet propulsion system for CubeSats

K Nishii, J Asakawa, K Kikuchi, M Akiyama… - Transactions of the …, 2020 - jstage.jst.go.jp
The University of Tokyo has proposed a water resistojet thruster with a high certainty of
liquid–vapor separation and low power consumption. In this propulsion system, liquid water …