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Genetic Programming Guidance for the Reentry Trajectory of the ReFEx Vehicle

Marchetti, Francesco and Redondo Gutierrez, Jose Luis and Seelbinder, David (2024) Genetic Programming Guidance for the Reentry Trajectory of the ReFEx Vehicle. In: 2024 IAF Space Transportation Solutions and Innovations Symposium at the 75th International Astronautical Congress, IAC 2024. 75th International Astronautical Congress (IAC), 2024-10-14 - 2024-10-18, Mailand, Italien. ISSN 0074-1795.

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Abstract

In this work Genetic Programming (GP) is used to obtain an alternative guidance law for online trajectory adaptation of the Reusability Flight Experiment (ReFEx) reentry vehicle. GP is an Evolutionary Algorithm (EA) capable of producing interpretable mathematical models that satisfies user defined objectives and constraints. It can be applied in a guidance setting, through direct interaction with the environment, learning to evolve a the guidance law to steer the vehicle towards the successful satisfaction of the mission. To the best of the authors' knowledge, the application of GP to a flight-ready vehicle represents a first in this domain and can help in increasing the TRL of this technique for Guidance and Control (G&C)applications. Furthermore, it produces interpretable models, in contrast to other Machine Learning (ML) approaches, and it can be applied to nonlinear models, in contrast with traditional methods.In this study, GP is applied offline to design an feedback guidance law to guide the ReFEx vehicle towards a desired final position in the presence of uncertainties in the physical models, navigation and control signals. The performance of the GP-based guidance law is compared against the current design, which defines the trajectory correction as an optimal control problem and reduces it to a nonlinear unconstrained optimization problem, which is then solved using a successive linearization strategy. The performance comparison between the two methods utilizes high fidelity 6-DoF Monte Carlo simulations. Capabilities, advantages and disadvantages of both methods are discussed and conclusions on the viability of the investigated GP approach are drawn.

Item URL in elib:https://elib.dlr.de/207659/
Document Type:Conference or Workshop Item (Speech)
Title:Genetic Programming Guidance for the Reentry Trajectory of the ReFEx Vehicle
Authors:
AuthorsInstitution or Email of AuthorsAuthor's ORCID iDORCID Put Code
Marchetti, FrancescoUNSPECIFIEDhttps://orcid.org/0000-0003-4552-0467184380918
Redondo Gutierrez, Jose LuisUNSPECIFIEDhttps://orcid.org/0000-0002-0037-2299UNSPECIFIED
Seelbinder, DavidUNSPECIFIEDUNSPECIFIEDUNSPECIFIED
Date:October 2024
Journal or Publication Title:2024 IAF Space Transportation Solutions and Innovations Symposium at the 75th International Astronautical Congress, IAC 2024
Refereed publication:No
Open Access:Yes
Gold Open Access:No
In SCOPUS:Yes
In ISI Web of Science:No
ISSN:0074-1795
Status:Published
Keywords:Genetic Programming, Reusable Launch Vehicle, Guidance, Machine Learning
Event Title:75th International Astronautical Congress (IAC)
Event Location:Mailand, Italien
Event Type:international Conference
Event Start Date:14 October 2024
Event End Date:18 October 2024
HGF - Research field:Aeronautics, Space and Transport
HGF - Program:Space
HGF - Program Themes:Space Transportation
DLR - Research area:Raumfahrt
DLR - Program:R RP - Space Transportation
DLR - Research theme (Project):R - Project ReFEx - Reusability Flight Experiment
Location: Bremen
Institutes and Institutions:Institute of Space Systems > Navigation and Control Systems
Deposited By: Marchetti, Francesco
Deposited On:20 May 2025 09:18
Last Modified:20 May 2025 09:18

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