NASA NTRS · 20120002557
Dual Accelerometer Usage Strategy for Onboard Space Navigation
Abstract
This work introduces a dual accelerometer usage strategy for onboard space navigation. In the proposed algorithm the accelerometer is used to propagate the state when its value exceeds a threshold and it is used to estimate its errors otherwise. Numerical examples and comparison to other accelerometer usage schemes are presented to validate the proposed approach.
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Zanetti, Renato, D'Souza, Chris. 2012-01-29. Dual Accelerometer Usage Strategy for Onboard Space Navigation. https://ntrs.nasa.gov/citations/20120002557
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