首页 | 本学科首页   官方微博 | 高级检索  
     检索      


Applications of multi-body dynamical environments: The ARTEMIS transfer trajectory design
Institution:1. National Aeronautics and Space Administration (NASA)/Goddard Space Flight Center, Greenbelt, MD, United States;2. Purdue University, West Lafayette, IN, United States;1. Department of Aerospace Engineering, The Pennsylvania State University, 229 Hammond Building, University Park, PA 16802, USA;2. Department of Mechanical and Aerospace Engineering, University of Strathclyde, James Weir Building, Glasgow G1 1XJ, United Kingdom;3. Department of Aerospace Engineering, University of Illinois at Urbana-Champaign, 302F Talbot Laboratory, 104 South Wright Street, Urbana, IL 61801, USA;1. Department of Civil and Industrial Engineering, University of Pisa, Pisa, Italy;2. Department of Astronautical, Electrical, and Energy Engineering, University of Rome “La Sapienza”, Rome, Italy;3. Italian Space Agency (ASI), Rome, Italy
Abstract:The application of forces in multi-body dynamical environments to permit the transfer of spacecraft from Earth orbit to Sun–Earth weak stability regions and then return to the Earth–Moon libration (L1 and L2) orbits has been successfully accomplished for the first time. This demonstrated that transfer is a positive step in the realization of a design process that can be used to transfer spacecraft with minimal Delta-V expenditures. Initialized using gravity assists to overcome fuel constraints; the ARTEMIS trajectory design has successfully placed two spacecrafts into Earth–Moon libration orbits by means of these applications.
Keywords:
本文献已被 ScienceDirect 等数据库收录!
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号