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dc.contributor.authorOland, Espen
dc.contributor.authorAndersen, Tom Stian
dc.date.accessioned2020-02-25T08:50:56Z
dc.date.available2020-02-25T08:50:56Z
dc.date.issued2019-07-22
dc.description.abstractThis paper presents preliminary results on how to perform waypoint tracking with spacecraft with actuator constraints. It considers a simplified spacecraft model and can be considered a deep space model, and shows how to perform waypoint tracking with only one main thruster together with full attitude control. As the spacecraft reaches close to the waypoint during a deceleration phase that makes the speed go towards zero, reaction control thrusters are used to make the remaining velocity error go to zero achieving the control objective.en_US
dc.identifier.citationOland, E., Andersen, T.S (2019) Preliminary Results on Waypoint Tracking for Spacecraft with Actuator Constraints. I <i> Proceedings of 9th International Conference on Recent Advances in Space Technologies (RAST), 2019</i>, IEEE, 239-244.en_US
dc.identifier.cristinIDFRIDAID 1796082
dc.identifier.doi10.1109/RAST.2019.8767812
dc.identifier.isbn978-1-5386-9448-0
dc.identifier.urihttps://hdl.handle.net/10037/17479
dc.language.isoengen_US
dc.publisherIEEE (Institute of Electrical and Electronics Engineers)en_US
dc.rights.accessRightsopenAccessen_US
dc.rights.holderCopyright 2019 The Author(s)en_US
dc.subjectVDP::Teknologi: 500::Elektrotekniske fag: 540::Andre elektrotekniske fag: 549en_US
dc.titlePreliminary Results on Waypoint Tracking for Spacecraft with Actuator Constraintsen_US
dc.type.versionacceptedVersionen_US
dc.typePeer revieweden_US
dc.typeChapteren_US
dc.typeBokkapittelen_US


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