SPACECRAFT SPIN AXIS ATTITUDE DETERMINATION

SPACECRAFT SPIN AXIS ATTITUDE DETERMINATION. IEEE TRANSACTIONS ON AEROSPACE AND ELECTRONIC SYSTEMS, 28. pp. 529-534.

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Abstract

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 computational requirements are discussed.

Item Type: Article
Subjects: Systems
Department: College of Computing and Mathematics > lndustrial and Systems Engineering
Depositing User: SYED AMEENUDDIN HUSSAIN
Date Deposited: 14 Jun 2008 10:39
Last Modified: 01 Nov 2019 13:44
URI: https://eprints.kfupm.edu.sa/id/eprint/2541