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Solar Sail Simplified Optimal Control Law for Reaching High Heliocentric Distances

Solar Sail Simplified Optimal Control Law for Reaching High Heliocentric Distances The aim of this paper is to analyze optimal trajectories of a solar sail-based spacecraft in missions towards the outer Solar System region. The paper proposes a simplified approach able to estimate the minimum flight time required to reach a given (sufficiently high) heliocentric distance. In particular, the effect of a set of solar photonic assists on the overall mission performance is analyzed with a simplified numerical approach. A comparison with results taken from the existing literature show the soundness of the proposed approach. http://www.deepdyve.com/assets/images/DeepDyve-Logo-lg.png Aerotecnica Missili & Spazio Springer Journals

Solar Sail Simplified Optimal Control Law for Reaching High Heliocentric Distances

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References (39)

Publisher
Springer Journals
Copyright
Copyright © AIDAA Associazione Italiana di Aeronautica e Astronautica 2021
ISSN
0365-7442
eISSN
2524-6968
DOI
10.1007/s42496-021-00100-7
Publisher site
See Article on Publisher Site

Abstract

The aim of this paper is to analyze optimal trajectories of a solar sail-based spacecraft in missions towards the outer Solar System region. The paper proposes a simplified approach able to estimate the minimum flight time required to reach a given (sufficiently high) heliocentric distance. In particular, the effect of a set of solar photonic assists on the overall mission performance is analyzed with a simplified numerical approach. A comparison with results taken from the existing literature show the soundness of the proposed approach.

Journal

Aerotecnica Missili & SpazioSpringer Journals

Published: Dec 1, 2021

Keywords: Solar sail; Trajectory optimization; Escape from the Solar System

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