Abstract
The validation of spacecraft flight nutation damping performance can only be obtained when flight data become available. Dedicated space nutation tests, e.g. in a decommissioning phase, are required to enable a systematic evaluation of model, ground test and space performance results. Space nutation flight data, however, are sparsely available. This article deals with the verification and validation of the COS-B and EQUATOR-S nutation flight data on basis of their ground test data and three model types. It will be shown that the Navier-Stokes model solution in the co-rotating body reference frame, as used in the development of the Ulysses, FY-2 and Cluster nutation dampers, is the backbone of liquid damper design of the type “tube-with-endpots”.
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Kuiper, H., Bongers, E. (2013). Flight Nutation Validation of the COS-B and EQUATOR-S Spacecraft. In: Chu, Q., Mulder, B., Choukroun, D., van Kampen, EJ., de Visser, C., Looye, G. (eds) Advances in Aerospace Guidance, Navigation and Control. Springer, Berlin, Heidelberg. https://doi.org/10.1007/978-3-642-38253-6_41
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DOI: https://doi.org/10.1007/978-3-642-38253-6_41
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