Dual Accelerometer Usage Strategy for Onboard Space Navigation | Zendy

Renato Zanetti | Zendy; Chris D’Souza | Zendy

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Dual Accelerometer Usage Strategy for Onboard Space Navigation

Author(s) -

Renato Zanetti,

Chris D’Souza

Publication year - 2012

Publication title -

journal of guidance control and dynamics

Language(s) - English

Resource type - Journals

SCImago Journal Rank - 1.573

H-Index - 143

eISSN - 1533-3884

pISSN - 0731-5090

DOI - 10.2514/1.58154

Subject(s) - accelerometer , computer science , dual (grammatical number) , space (punctuation) , remote sensing , aerospace engineering , aeronautics , engineering , geography , art , literature , operating system

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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