How can we increase the accuracy of determination of spacecraft׳s lifetime?

Author:

Nazarenko A.I.

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference11 articles.

1. A.I. Nazarenko, Determination and prediction of satellite motion at the end of the lifetime, in: Proceedings of the International Workshop on Salyut-7/Kosmos-1686 Reentry, ESOC, Darmstadt (G), 9 April 1991.

2. A.I. Nazarenko, A.G. Klimenko, Method for Determining and Forecasting the Spacecraft Motion on Low-Earth Orbits Subjected to the Effect of Drag in the Atmosphere, Patent for invention 2463223, Russian Federation, JSC Russian space systems, Application No. 2011112179, invention priority March 30, 2011.

3. A.I. Nazarenko, V. S. Yurasov, K. T. Alfriend, P. J. Cefola, Optimal measurement filtering and motion prediction taking into account the atmospheric perturbations, in: Proceedings of the AAS/AIAA Astrodynamics Specialist Conference, Mackinac Island, Michigan, Paper AAS 07-363.

4. A.I. Nazarenko, Estimate of the GOCE SC lifetime termination, Site “satmotion.ru”, 2013.

5. Application of the method for optimum filtering of measurements for determination and prediction of spacecraft orbits;Nazarenko;Sol. Syst. Res.,2013

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