Low-thrust trajectory design with successive convex optimization for libration point orbits
Y Kayama, KC Howell, M Bando… - Journal of Guidance …, 2022 - arc.aiaa.org
In space missions, numerical techniques for minimizing the fuel consumption of spacecraft
using low-thrust propulsion are desirable. Among various nonlinear optimization methods …
using low-thrust propulsion are desirable. Among various nonlinear optimization methods …
Motion Primitive Approach to Spacecraft Trajectory Design in the Neptune-Triton System
The identification of the Neptunian system as a high-priority target for future missions
motivates the design of trajectories that can deliver a spacecraft from a high-energy …
motivates the design of trajectories that can deliver a spacecraft from a high-energy …
Minimum fuel trajectory design using sparse optimal control in three-body problem
Y Kayama, M Bando, S Hokamoto - AIAA Scitech 2020 Forum, 2020 - arc.aiaa.org
This study formulates a successive multiple sparse optimal control method to minimize a fuel
consumption of spacecraft in three-body problem. This method uses a convex optimization …
consumption of spacecraft in three-body problem. This method uses a convex optimization …
Near-Earth Asteroids Fly-By Trajectory Optimization For Mining Purposes
M Bruno - 2024 - webthesis.biblio.polito.it
The diminishing availability of Earth's resources has catalyzed the emergence of space
mining as a burgeoning industry, with the recent success of missions like OSIRIS-REx …
mining as a burgeoning industry, with the recent success of missions like OSIRIS-REx …
[PDF][PDF] Optimal Trajectory Design and Control for Low-Thrust Spacecraft in Multi-Body Dynamics
香山裕樹 - 2021 - catalog.lib.kyushu-u.ac.jp
1.1 Background The first satellite Sputnik 1 developed by the Soviet Union was launched
into outer space in 1957 [1]. Since then, numerous satellites and spacecraft have been …
into outer space in 1957 [1]. Since then, numerous satellites and spacecraft have been …