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SPACECRAFT SPIN AXIS ATTITUDE DETERMINATION

Emara-Shabaik, Husam 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
Divisions:College Of Computer Sciences and Engineering > Systems Engineering Dept
Creators:Emara-Shabaik, Husam
Email:Shabaik@kfupm.edu.sa
ID Code:2541
Deposited By:SYED AMEENUDDIN HUSSAIN
Deposited On:14 Jun 2008 13:39
Last Modified:12 Apr 2011 13:13

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