Theory of Functional Connections and Nelder-Mead optimization methods applied in satellite characterization

TL;DR

This paper compares two optimization methods, the Theory of Functional Connections and Nelder-Mead, for satellite parameter estimation from observational data, enhancing space debris monitoring and astronomical observations.

Contribution

It introduces the application of TFC and Nelder-Mead to satellite dynamics, providing a novel approach for data embedding and parameter estimation in space object characterization.

Findings

TFC ensures observational data constraints are always satisfied.

Nelder-Mead offers a gradient-free optimization alternative.

Both methods' accuracy and efficiency are evaluated across models.

Abstract

The growing population of man-made objects with the build up of mega-constellations not only increases the potential danger to all space vehicles and in-space infrastructures (including space observatories), but above all poses a serious threat to astronomy and dark skies. Monitoring of this population requires precise satellite characterization, which is is a challenging task that involves analyzing observational data such as position, velocity, and light curves using optimization methods. In this study, we propose and analyze the application of two optimization procedures to determine the parameters associated with the dynamics of a satellite: one based on the Theory of Functional Connections (TFC) and another one based on the Nelder-Mead heuristic optimization algorithm. The TFC performs linear functional interpolation to embed the constraints of the problem into a functional. In this paper, we propose to use this functional to analytically embed the observational data of a satellite into its equations of dynamics. After that, any solution will always satisfy the observational data. The second procedure proposed in this research takes advantage of the Nealder-Mead algorithm, that does not require the gradient of the objective function, as alternative solution. The accuracy, efficiency, and dependency on the initial guess of each method is investigated, analyzed, and compared for several dynamical models. These methods can be used to obtain the physical parameters of a satellite from available observational data and for space debris characterization contributing to follow-up monitoring activities in space and astronomical observatories.