Maneuver Design Using Relative Orbital Elements
作者: David A. SpencerThomas A. Lovell
作者单位: 1Georgia Institute of Technology
2Air Force Research Laboratory
刊名: The Journal of the Astronautical Sciences, 2015, Vol.62 (4), pp.315-350
来源数据库: Springer Journal
DOI: 10.1007/s40295-015-0072-y
关键词: Orbital mechanicsRelative motionProximity operations
英文摘要: Abstract(#br)Relative orbital elements provide a geometric interpretation of the motion of a deputy spacecraft about a chief spacecraft. The formulation yields an intuitive understanding of how the relative motion evolves with time, and by incorporating velocity changes in the local-vertical, local-horizontal component directions, the change in relative motion due to impulsive maneuvers can be evaluated. This paper utilizes a relative orbital element formulation that characterizes relative motion where the chief spacecraft is assumed to be in a circular orbit. Expressions are developed for changes to the relative orbital elements as a function of the impulsive maneuver components in each coordinate direction. A general maneuver strategy is developed for targeting a set of relative orbital...
全文获取路径: PDF下载  Springer  (合作)
分享到:
来源刊物:
影响因子:0.697 (2012)

×