Spacecraft Spin Axis Attitude Determination

H. E. Emara-Shabaik*

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

4 Scopus citations

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.

Original languageEnglish
Pages (from-to)529-534
Number of pages6
JournalIEEE Transactions on Aerospace and Electronic Systems
Volume28
Issue number2
DOIs
StatePublished - Apr 1992

ASJC Scopus subject areas

  • Aerospace Engineering
  • Electrical and Electronic Engineering

Fingerprint

Dive into the research topics of 'Spacecraft Spin Axis Attitude Determination'. Together they form a unique fingerprint.

Cite this