Orbit maintenance of quasi-satellite trajectories via mean relative orbit elements

dc.contributor.authorBaresi, Nicola
dc.contributor.authorDell'Elce, Lamberto
dc.contributor.authorDos Santos, Josué Cardoso
dc.contributor.authorKawakatsu, Yasuhiro
dc.contributor.institutionISAS/JAXA
dc.contributor.institutionSophia Antipolis
dc.contributor.institutionSão Paulo State University
dc.date.accessioned2022-04-28T19:27:10Z
dc.date.available2022-04-28T19:27:10Z
dc.date.issued2018-01-01
dc.description.abstractThe Martian Moons eXploration mission is currently under development at JAXA and will be the first spacecraft mission to retrieve pristine samples from the surface of Phobos. In preparation for the sampling operations, MMX will collect observations of Phobos from stable retrograde relative trajectories also known as quasi-satellite orbits or QSOs. This paper offers a semi-analytical analysis of mid- and high-altitude QSOs in terms of relative orbit elements. Our analysis is not limited to planar orbits and takes into account the eccentricity of the moon's orbit. Furthermore, we introduce a numerical map between mean and osculating orbit elements to study the long-term evolution of MMX and derive a Lyapunov control law for orbit maintenance purposes. The nonlinear controller is based on mean relative orbit element differences and tested with respect to injection errors.en
dc.description.affiliationISAS/JAXA
dc.description.affiliationUniversité Côte d'Azur and Inria Sophia Antipolis
dc.description.affiliationSão Paulo State University
dc.identifier.citationProceedings of the International Astronautical Congress, IAC, v. 2018-October.
dc.identifier.issn0074-1795
dc.identifier.scopus2-s2.0-85065308900
dc.identifier.urihttp://hdl.handle.net/11449/221295
dc.language.isoeng
dc.relation.ispartofProceedings of the International Astronautical Congress, IAC
dc.sourceScopus
dc.titleOrbit maintenance of quasi-satellite trajectories via mean relative orbit elementsen
dc.typeTrabalho apresentado em evento

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