An analytical theory for avoidance collision between space debris and operating satellites in LEO-Reference-Cited by-同舟云学术

An analytical theory for avoidance collision between space debris and operating satellites in LEO

Published:2013-10 Issue:18-19 Volume:37 Page:8283-8291
ISSN:0307-904X
Container-title:Applied Mathematical Modelling
language:en
Short-container-title:Applied Mathematical Modelling

Author:

Abdel-Aziz Yehia A.

Publisher

Elsevier BV

Subject

Applied Mathematics,Modeling and Simulation

Reference19 articles.

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3. F.R. Hoots, R.L. Roehrich, Models for propagation of NORAD element sets, Spacetrack, Report No. 3, 1988.

4. Orbital evaluoation of space debris;Wnuk;Adv. Space Res.,2001

5. An efficient algorithm for orbital evolution of artificial satellite;Abdel-Aziz;Appl. Math. Comput.,2007

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