SPACECRAFT SPIN AXIS ATTITUDE DETERMINATION

This paper provides a mathematical formulation and two solution algorithms of the problem of spacecraft spin axis attitude determination from noisy measurements.The two developed algorithms are compared through digital simulation and their relative merits in terms of estimation accuracy and computat...

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Bibliographic Details
Main Author: Emara-Shabaik, Husam (author)
Other Authors: unknown (author)
Format: article
Published: 2020
Subjects:
Online Access:https://eprints.kfupm.edu.sa/id/eprint/2541/1/15.pdf
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