[HTML][HTML] Launch and deployment of distributed small satellite systems

NH Crisp, K Smith, P Hollingsworth - Acta Astronautica, 2015 - Elsevier
The rise in launch and use of small satellites in the past decade, a result of improved
functionality through technology miniaturisation and alternative design philosophies, has …

Satellite formation flying for an interferometry mission

JA Roberts - 2005 - dspace.lib.cranfield.ac.uk
The autonomous formation flying of multiple spacecraft to replace a single large satellite will
be an enabling technology for many future missions. In this research, the current status of …

A new constellation configuration scheme for communicating architecture in cislunar space

M Xu, J Wang, S Liu, S Xu - Mathematical Problems in …, 2013 - Wiley Online Library
A new constellation configuration is proposed to provide near‐constant communications
between any two points in the cislunar space. Four satellites were allocated on some natural …

地月L2 点周期轨道的月球背面覆盖分析

刘磊, 曹建峰, 胡松杰, 唐歌实 - 深空探测学报(中英文), 2017 - jdse.bit.edu.cn
地月L2 点附近轨道具备独特的动力学和运动学特性, 是月球背面探测任务的中继卫星首选布设
位置. 面向未来月球背面探测任务的中继通信需求, 分析并研究了地月L2 点周期轨道(halo 轨道) …

Satellite constellation build-up via three-body dynamics

MJ Nadoushan, AB Novinzadeh - Proceedings of the …, 2014 - journals.sagepub.com
In this article, a method for satellite constellation build-up is presented based on three-body
dynamics. This method enables satellite constellation build-up with single launch and less …

Multi-phase mission analysis and design for satellite constellations with low-thrust propulsion

S Huang - 2020 - politesi.polimi.it
As the demand for services from Space is more and more important to life on the Earth, the
international interest in satellite constellations is increasingly growing. For example, in the …

Maintenance of earth-moon halo orbit

L Liu, C Hu, M Wang, Y Wang - 2017 36th Chinese Control …, 2017 - ieeexplore.ieee.org
Halo orbit nearby the Earth-Moon libration points is valuable to explore the lunar farside,
which however must frequently be controlled to stay in the vicinity of libration points because …

CHANG'E-3 contingency scheme and trajectory

L Liu, J Cao, Y Liu, S Hu, G Tang, J Xie - Advances in Space Research, 2015 - Elsevier
This paper addresses contingency trajectories of CHANG'E-3 in the case of a failure of the
lunar brake, which is crucial to the CHANG'E-3 mission, ie, the first Chinese lunar soft …

The optimization of transfer trajectory for small amplitude halo orbits

LI Ming-Tao, Z Jian-Hua - Measurement and Control, 2008 - journals.sagepub.com
Since the halo orbits in the vicinity of the collinear libration points have a strong hyperbolic
character, it is possible to use their stable manifold for the transfer from the Earth. However …

Coverage of lunar farside surface of the Earth-Moon L2 periodic orbits

LIU Lei, CAO Jianfeng, H Songjie… - Journal of Deep Space …, 2017 - jdse.bit.edu.cn
Abstract Orbits nearby the Earth-Moon libration points have the specific dynamic
characteristicsand are the preferred position of relay satellites for the lunar farside …