Abstract ESA Solar Orbiter was launched from Cape Canaveral in collaboration with NASA on the February 10, 2020 to start its journey around the Sun, with the commissioning phase ending in April 2020. After commissioning, ESA set a tighter pointing requirement goal to further improve the performance in Fine Pointing Mode, in preparation of the upcoming start of Science Phase. The first part of this paper outlines the end-to-end process which allowed - in just six months – to update the Fine Pointing Mode Design, re-tune the controller with refined assumptions taken from flight data and robust methods and execute full validation of the new AOCS Software on the Avionics Test bench at Airbus Defence and Space. The second part of the paper describes the upload in flight of the new Software and the analysis of the on-orbit pointing performance, which showed a significant improvement with respect to the previous one, thus contributing to the success of the Mission's scientific goals.
Highlights Solar Orbiter Payload Instruments required a better pointing jitter performance (Relative Pointing Error) after launch Root cause analysis on flight telemetry to identify driver contributors to pointing error Fine Pointing Mode controller design and tuning updated with refined inputs based on flight data and with robust control methods Controller uploaded in flight significantly improved the Spacecraft pointing performance
Solar Orbiter fine pointing Mode improvement in flight: Challenges and achievements
Acta Astronautica ; 213 ; 264-276
2023-09-14
13 pages
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Orbiter Motion - Microgravity and pointing
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