Trajectory design for kuiper belt mission using multiple gravity assists

Boqin Hu*, Dong Qiao, Xiangyu Li, Qi Chen

*Corresponding author for this work

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

The Kuiper belt is a circumstellar disc in the outer Solar System, which consists mainly of small bodies or remnants originated from the beginning of the formation of the Solar System. While many asteroids are composed primarily of rocks and metals, most Kuiper belt objects are largely composed of frozen volatiles. These ancient materials could provide insights into the early history of the Solar System. In this study, a series of trajectories are designed for targets of Kuiper Belt missions using multiple gravity assists, departing from Earth between 2018 and 2050 based on the traditional flyby mission architecture. For fast missions, planetary gravity-assisted model associated with the differential evolution algorithm is used to design the trajectories to targets. For time-free exploration missions, based on the multiple gravity-assisted model and the global hybrid optimization algorithm, the multiple gravity-assisted trajectories to the targets of Kuiper belt missions are designed. The results of this paper can provide references to the trajectory design for Kuiper belt exploration in the future.

Original languageEnglish
Title of host publicationDynamics and Control of Space Systems
EditorsJeng-Shing Chern, Ya-Zhong Luo, Xiao-Qian Chen, Lei Chen
PublisherUnivelt Inc.
Pages1343-1351
Number of pages9
ISBN (Print)9780877036531
Publication statusPublished - 2018
Event4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018 - Changsha, China
Duration: 21 May 201823 May 2018

Publication series

NameAdvances in the Astronautical Sciences
Volume165
ISSN (Print)0065-3438

Conference

Conference4th IAA Conference on Dynamics and Control of Space Systems, DYCOSS 2018
Country/TerritoryChina
CityChangsha
Period21/05/1823/05/18

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