dc.contributor.author | McGhan, Catharine L. R. | |
dc.contributor.author | Murray, Richard M. | |
dc.contributor.author | Serra, Romain | |
dc.contributor.author | Ingham, Michel D. | |
dc.contributor.author | Ono, Masahiro | |
dc.contributor.author | Estlin, Tara | |
dc.contributor.author | Williams, Brian C | |
dc.date.accessioned | 2017-05-02T20:37:38Z | |
dc.date.available | 2017-05-02T20:37:38Z | |
dc.date.issued | 2015-06 | |
dc.date.submitted | 2015-03 | |
dc.identifier.isbn | 978-1-4799-5379-0 | |
dc.identifier.isbn | 978-1-4799-5380-6 | |
dc.identifier.uri | http://hdl.handle.net/1721.1/108617 | |
dc.description.abstract | In this paper we discuss a resilient, risk-aware software architecture for onboard, real-time autonomous operations that is intended to robustly handle uncertainty in space-craft behavior within hazardous and unconstrained environments, without unnecessarily increasing complexity. This architecture, the Resilient Spacecraft Executive (RSE), serves three main functions: (1) adapting to component failures to allow graceful degradation, (2) accommodating environments, science observations, and spacecraft capabilities that are not fully known in advance, and (3) making risk-aware decisions without waiting for slow ground-based reactions. This RSE is made up of four main parts: deliberative, habitual, and reflexive layers, and a state estimator that interfaces with all three. We use a risk-aware goal-directed executive within the deliberative layer to perform risk-informed planning, to satisfy the mission goals (specified by mission control) within the specified priorities and constraints. Other state-of-the-art algorithms to be integrated into the RSE include correct-by-construction control synthesis and model-based estimation and diagnosis. We demonstrate the feasibility of the architecture in a simple implementation of the RSE for a simulated Mars rover scenario. | en_US |
dc.language.iso | en_US | |
dc.publisher | Institute of Electrical and Electronics Engineers (IEEE) | en_US |
dc.relation.isversionof | http://dx.doi.org/10.1109/AERO.2015.7119035 | en_US |
dc.rights | Creative Commons Attribution-Noncommercial-Share Alike | en_US |
dc.rights.uri | http://creativecommons.org/licenses/by-nc-sa/4.0/ | en_US |
dc.source | Other univ. web domain | en_US |
dc.title | A risk-aware architecture for resilient spacecraft operations | en_US |
dc.type | Article | en_US |
dc.identifier.citation | .McGhan, Catharine L. R. et al. “A Risk-Aware Architecture for Resilient Spacecraft Operations.” 2015 IEEE Aerospace Conference, 7-14 March, 2015, Big Sky, MT, USA, IEEE, 2015. 1–15. | en_US |
dc.contributor.department | Massachusetts Institute of Technology. Department of Aeronautics and Astronautics | en_US |
dc.contributor.mitauthor | Williams, Brian C | |
dc.relation.journal | 2015 IEEE Aerospace Conference | en_US |
dc.eprint.version | Author's final manuscript | en_US |
dc.type.uri | http://purl.org/eprint/type/ConferencePaper | en_US |
eprint.status | http://purl.org/eprint/status/NonPeerReviewed | en_US |
dspace.orderedauthors | McGhan, Catharine L. R.; Murray, Richard M.; Serra, Romain; Ingham, Michel D.; Ono, Masahiro; Estlin, Tara; Williams, Brian C. | en_US |
dspace.embargo.terms | N | en_US |
dc.identifier.orcid | https://orcid.org/0000-0002-1057-3940 | |
mit.license | OPEN_ACCESS_POLICY | en_US |