A constant gain Kalman filter approach for the prediction of re-entry of risk objects-Reference-Cited by-同舟云学术

A constant gain Kalman filter approach for the prediction of re-entry of risk objects

Published:2007-11 Issue:10 Volume:61 Page:831-839
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Anilkumar A.K.,Ananthasayanam M.R.,Subba Rao P.V.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference20 articles.

1. A.K. Anilkumar, New perspectives for analyzing the breakup, environment, evolution, collision risk and reentry of space debris objects, Ph.D. Thesis, 〈http://etd.ncsi.iisc.ernet.in/handle/2005/80〉, Department of Aerospace Engineering, Indian Institute of Science, Bangalore, India, 2004.

2. Artificial Space Debris;Johnson,1987

3. Web sites for two line element sets 〈http://www.geocities.com/iss25544/#TLEs〉 or 〈http://www.wingar.demon.co.uk〉 or 〈http://www.celestrak.com〉.

4. Satellite Orbits in an Atmosphere: Theory and Applications;King-Hele,1987

5. Fundamentals of Astrodynamics and Applications;Vallado,2001

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