Trajectory Design for Proximity Operations: The Relative Orbital Elements' Perspective
Description
The data sets provided here can be used to recreate the plots of the paper “Trajectory Design for Proximity Operations: The Relative Orbital Elements’ Perspective” available at this link.
That paper presents how to rigorously transform back-and-forth the equations of the relative motion in the close-range regime between Hill-Clohessy-Wiltshire and Relative Orbital Elements formulations. As straightforward application, it is presented a methodology to generate piecewise constant acceleration profiles from an impulsive guidance solution, setting up a control grid that minimizes the difference between impulsive and equivalent delta-v burns corresponding to the acceleration profile.
Applications are implementation of autonomous guidance and control policies for close-range satellite proximity operations.
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Additional details
Related works
- Is supplement to
- Journal article: 10.2514/1.G006175 (DOI)
References
- Gaias, G., & Lovera, M.. (2021). Trajectory Design for Proximity Operations: The Relative Orbital Elements' Perspective. [Data set] Zenodo. http://doi.org/10.5281/zenodo.5592594