Publication Type:

Journal Article

Source:

International Journal of Applied Engineering Research, Research India Publications, Volume 9, Number 14, p.2733-2744 (2014)

URL:

http://www.scopus.com/inward/record.url?eid=2-s2.0-84901236298&partnerID=40&md5=7b98feac3111f7b1965b65bf2a4e3ee5

Abstract:

<p>The attitude determination of a spacecraft has attracted the attention of many researchers over the years. Attitude determination is a crucial part in implementation of reliable control systems for spacecraft. Attitude determination algorithms are broadly classified into two classes, deterministic algorithms and recursive estimation algorithms [12]. This paper aims to advantageously combine these two algorithms FOAM (a deterministic algorithm) and Kalman filtering (a recursive estimation algorithm) to give a more accurate estimate of spacecraft attitude by overcoming inherent sensor errors. © Research India Publications.</p>

Notes:

cited By (since 1996)0

Cite this Research Publication

GaDeeptha Shree, Singh, Va, Dai, B. Kb, and Sunitha, Ra, “Attitude determination of spacecraft using FOAM and Kalman filtering”, International Journal of Applied Engineering Research, vol. 9, pp. 2733-2744, 2014.