A Sliding Mode Control-Based Guidance Law for a Two-Dimensional Orbit Transfer with Bounded Disturba...
A Sliding Mode Control-Based Guidance Law for a Two-Dimensional Orbit Transfer with Bounded Disturbances
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Basel: MDPI AG
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Language
English
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Basel: MDPI AG
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The aim of this paper is to analyze the performance of a state-feedback guidance law, which is obtained through a classical sliding mode control approach, in a two-dimensional circle-to-circle orbit transfer of a spacecraft equipped with a continuous-thrust propulsion system. The paper shows that such an inherently robust control technique can be e...
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A Sliding Mode Control-Based Guidance Law for a Two-Dimensional Orbit Transfer with Bounded Disturbances
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TN_cdi_doaj_primary_oai_doaj_org_article_cacd6a0791654a1da700251836bbe7b7
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https://devfeature-collection.sl.nsw.gov.au/record/TN_cdi_doaj_primary_oai_doaj_org_article_cacd6a0791654a1da700251836bbe7b7
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ISSN
2076-0825
E-ISSN
2076-0825
DOI
10.3390/act12120444
