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.
Dual Accelerometer Usage Strategy for Onboard Space Navigation
2012
11 pages
Report
No indication
English
ENGINEERING NOTES - Dual Accelerometer Usage Strategy for Onboard Space Navigation
Online Contents | 2012
|Dual Accelerometer Usage Strategy for Onboard Space Navigation (AAS 12-198)
British Library Conference Proceedings | 2012
|Onboard navigation of the Space Shuttle
NTRS | 1975
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