Modeling Reaction-Control-System Effects on Mars Odyssey

Modeling Reaction-Control-System Effects on Mars Odyssey

During the Mars 2001 Odyssey aerobraking mission, NASA Langley Research Center performed six-degree-of-freedom simulations to model rotational motion of the spacecraft. The main objective of this study was to assess the reaction-control-system models and their effects on the atmospheric flight of Od...

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Veröffentlicht in:Journal of spacecraft and rockets 2005-05, Vol.42 (3), p.444-449
Hauptverfasser: Prince, Jill L. Hanna, Chavis, Zachary Q, Wilmoth, Richard G
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Mars Odyssey Mission (NASA)
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container_title Journal of spacecraft and rockets
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creator Prince, Jill L. Hanna
Chavis, Zachary Q
Wilmoth, Richard G
description During the Mars 2001 Odyssey aerobraking mission, NASA Langley Research Center performed six-degree-of-freedom simulations to model rotational motion of the spacecraft. The main objective of this study was to assess the reaction-control-system models and their effects on the atmospheric flight of Odyssey. Based on these models, a comparison was made between data derived from flight measurements to simulated rotational motion of the spacecraft during aerobraking at Mars. The differences between the simulation and flight-derived Odyssey data were then used to adjust the model aerodynamic parameters as a result of reaction-control-system firings to achieve a better correlation.
doi_str_mv 10.2514/1.15198
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subjects Mars Odyssey Mission (NASA)
title Modeling Reaction-Control-System Effects on Mars Odyssey
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