Abstract The International Rosetta Mission was launched on 2nd March 2004 on its 10 years journey to comet 67P/Churyumov–Gerasimenko. Rosetta will reach the comet in 2014, orbit it for about 1.5 years down to distances of a few kilometres and deliver the Lander Philae onto its surface. Following the fly-by of Asteroid (21-)Lutetia in 2010, Rosetta continued its travel towards the planned comet encounter in 2014. In this phase Rosetta became the solar-powered spacecraft that reached the largest Sun distances in history of spaceflight, up to an aphelion at 5.3AU in October 2012. At distances above 4.5AU the spacecraft's solar generator power is not sufficient to keep all spacecraft systems active. Therefore in June 2011 the spacecraft was spun up to provide gyroscopic stabilisation, and most of its on-board units, including those used for attitude control and communications, were switched off. Over this “hibernation” phase of about 2.5 years the spacecraft will keep a minimum of autonomy active to ensure maintenance of safe thermal conditions. After Lutetia fly-by, flight controllers had to tackle two anomalies that had significant impacts on the mission operations. A leak in the reaction control subsystem was confirmed and led to the re-definition of the operational strategy to perform the comet rendezvous manoeuvres planned for 2011 and 2014. Anomalous jumps detected in the estimated friction torque of two of the four reaction wheels used for attitude control forced the rapid adoption of measures to slow down the wheels degradation. This included in-flight re-lubrication activities and changes in the wheels operational speed regime. Once the troubleshooting of the two anomalies was completed, and the related operational scenarios were implemented, the first large (790m/s) comet rendezvous manoeuvre was executed, split into several long burns in January and February 2011. The second burn was unexpectedly interrupted due to the anomalous behaviour of two thrusters, causing attitude off-pointing. Flight controllers modified the thrusters operation parameters in the on-board software and managed to re-start the sequence of burns and successfully complete the manoeuvre. After the manoeuvre, preparation for the critical spin-up and hibernation entry activities, planned for June 2011, began. This paper presents the activities carried out on Rosetta in the final year before hibernation entry. The major anomalies and the related troubleshooting and workaround solutions are detailed. Lessons learned from the operation of the first spacecraft operating with solar power at Jupiter-like distances from the Sun are presented and discussed.

    Highlights ► Last critical Rosetta operations before 2.5 years hibernation are described. ► Problems with pressurisation worked around thanks to good fuel margins available. ► Anomalous thrusters behaviour forced reprogramming of the on-board modulator. ► Hibernation entry performed with strobing RF carrier as only the spacecraft feedback.


    Zugriff

    Zugriff prüfen

    Verfügbarkeit in meiner Bibliothek prüfen

    Bestellung bei Subito €


    Exportieren, teilen und zitieren



    Titel :

    Rosetta enters hibernation


    Beteiligte:

    Erschienen in:

    Acta Astronautica ; 79 ; 124-130


    Erscheinungsdatum :

    2012-04-26


    Format / Umfang :

    7 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch




    Rosetta enters hibernation

    Ferri, Paolo | Online Contents | 2012


    Space mission hibernation mode design: Lessons learned from Rosetta and other pathfinding missions using hibernation

    West, John L. / Accomazzo, Andrea / Chmielewski, Arthur B. et al. | IEEE | 2018



    Rosetta Lander—After seven years of cruise, prepared for hibernation

    Ulamec, Stephan / Biele, Jens / Fantinati, Cinzia et al. | Elsevier | 2012


    Hibernation storage testing of a reaction wheel for the ROSETTA programme

    McMahon, P. / European Space Agency / University of Liege | British Library Conference Proceedings | 2001