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The Journal of the Astronautical Sciences

, Volume 62, Issue 4, pp 315–350 | Cite as

Maneuver Design Using Relative Orbital Elements

  • David A. SpencerEmail author
  • Thomas A. Lovell
Article

Abstract

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 elements, and this strategy is applied to scenarios that are relevant for close proximity operations, including establishing a stationary relative orbit, natural motion circumnavigation, and station-keeping in a leading or trailing orbit.

Keywords

Orbital mechanics Relative motion Proximity operations 

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Copyright information

© American Astronautical Society 2015

Authors and Affiliations

  1. 1.Guggenheim School of Aerospace EngineeringGeorgia Institute of TechnologyAtlantaUSA
  2. 2.Space Vehicles DirectorateAir Force Research LaboratoryKirtlandUSA

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