Parametric Optimization of Low Thrust Orbital Maneuvers

TL;DR

This paper presents a numerical analysis of parametric optimization techniques for low thrust orbital maneuvers, focusing on how prescribed thrust laws influence orbital correction efficiency.

Contribution

It introduces a systematic approach to optimize low thrust maneuvers under specific thrust direction constraints, advancing orbital maneuver planning methods.

Findings

Optimized thrust laws improve fuel efficiency.

Parametric constraints significantly affect maneuver outcomes.

Numerical methods enable precise control of low thrust trajectories.

Abstract

The goal of the present paper is to make a numerical analysis of parametric optimization of low thrust orbital maneuver. An orbital maneuver occurs when it is necessary to modify the orbit a space vehicle to change its function or to correct effects of perturbations. A parametric optimization is made when the thrust is not free to point to any direction, but has to follow some prescribed law, like a linear or quadratic relation with time.