Artigo Acesso aberto

Autonomous Satellite Rendezvous and Proximity Operations with Time-Constrained Sub-Optimal Model Predictive Control

2023; Elsevier BV; Volume: 56; Issue: 2 Linguagem: Inglês

10.1016/j.ifacol.2023.10.228

ISSN

2405-8971

Autores

Gabriel Behrendt, Alexander A. Soderlund, Matthew Hale, Sean Phillips,

Tópico(s)

Astro and Planetary Science

Resumo

This paper presents a time-constrained model predictive control strategy for the 6 degree-of-freedom (6DOF) autonomous rendezvous and docking problem between a controllable "deputy" spacecraft and an uncontrollable "chief" spacecraft. The control strategy accounts for computational time constraints due to limited onboard processing speed. The translational dynamics model is derived from the Clohessy-Wiltshire equations and the angular dynamics are modeled on gas jet actuation about the deputy's center of mass. Simulation results are shown to achieve the docking configuration under computational time constraints by limiting the number of allowed algorithm iterations when computing each input. Specifically, we show that upwards of 90% of computations can be eliminated from a model predictive control implementation without significantly harming control performance.

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