Sliding-Mode Control for On-Orbit Rendezvous with a Fleeing Passive Target on a Circular Capture Trajectory
dc.rights.license | open | en_US |
hal.structure.identifier | Laboratoire de l'intégration, du matériau au système [IMS] | |
dc.contributor.author | HENRY, David | |
dc.contributor.author | DE LOZA, Alejandra Ferreira | |
hal.structure.identifier | Laboratoire de l'intégration, du matériau au système [IMS] | |
dc.contributor.author | FAURE, Martin | |
hal.structure.identifier | Laboratoire de l'intégration, du matériau au système [IMS] | |
dc.contributor.author | CIESLAK, Jerome
IDREF: 11916406X | |
dc.contributor.author | PUNTA, Elisabetta | |
dc.date.accessioned | 2023-05-30T07:37:40Z | |
dc.date.available | 2023-05-30T07:37:40Z | |
dc.date.issued | 2022-08-01 | |
dc.date.conference | 2022-06-28 | |
dc.identifier.issn | 2473-2001 | en_US |
dc.identifier.uri | https://oskar-bordeaux.fr/handle/20.500.12278/182353 | |
dc.description.abstractEn | This paper deals with the design of finite-time controllers for on-orbit rendezvous and capture missions. The objective is to assess the capacity of sliding–mode controllers to control a chaser spacecraft during a capture maneuver of a fleeing passive spacecraft. The control solution is based on a variable structure approach that relies on the sliding mode control theory. More precisely, the general super-twisting algorithm is used to control the chaser’s attitude, whereas the control of the relative position between the two spacecraft is based on the simplex-based sliding mode control theory. The method is tested in a full-scaled benchmark that accurately simulates the capture mission. | |
dc.language.iso | EN | en_US |
dc.subject | Space vehicles | |
dc.subject | Automation | |
dc.subject | Attitude control | |
dc.subject | Propulsion | |
dc.subject | Benchmark testing | |
dc.subject | Harmonic analysis | |
dc.subject | Orbits | |
dc.subject | Position control | |
dc.subject | Space vehicles | |
dc.subject | Variable structure systems | |
dc.title.en | Sliding-Mode Control for On-Orbit Rendezvous with a Fleeing Passive Target on a Circular Capture Trajectory | |
dc.type | Communication dans un congrès avec actes | en_US |
dc.identifier.doi | 10.1109/MED54222.2022.9837287 | en_US |
dc.subject.hal | Sciences de l'ingénieur [physics]/Automatique / Robotique | en_US |
bordeaux.page | 571-576 | en_US |
bordeaux.hal.laboratories | IMS : Laboratoire de l'Intégration du Matériau au Système - UMR 5218 | en_US |
bordeaux.institution | Université de Bordeaux | en_US |
bordeaux.institution | Bordeaux INP | en_US |
bordeaux.institution | CNRS | en_US |
bordeaux.conference.title | 30th IEEE Mediterranean Conference on Control and Automation, Jun 2022, Athens, Greece. | en_US |
bordeaux.country | gr | en_US |
bordeaux.title.proceeding | 2022 30th Mediterranean Conference on Control and Automation (MED) | en_US |
bordeaux.team | AUTOMATIQUE-ARIA | en_US |
bordeaux.conference.city | Athènes | en_US |
bordeaux.peerReviewed | oui | en_US |
hal.export | false | |
dc.rights.cc | Pas de Licence CC | en_US |
bordeaux.COinS | ctx_ver=Z39.88-2004&rft_val_fmt=info:ofi/fmt:kev:mtx:journal&rft.date=2022-08-01&rft.spage=571-576&rft.epage=571-576&rft.eissn=2473-2001&rft.issn=2473-2001&rft.au=HENRY,%20David&DE%20LOZA,%20Alejandra%20Ferreira&FAURE,%20Martin&CIESLAK,%20Jerome&PUNTA,%20Elisabetta&rft.genre=proceeding |
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