Analytical solution to the perturbedJ 2 motion of Artificial Satellite in terms of Euler parameters-Reference-Cited by-同舟云学术

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Analytical solution to the perturbedJ 2 motion of Artificial Satellite in terms of Euler parameters

Published:1995 Issue:1 Volume:69 Page:1-12
ISSN:0167-9295
Container-title:Earth, Moon, and Planets
language:en
Short-container-title:Earth Moon Planet

Author:

Awad Mervat El-Sayed

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Earth and Planetary Sciences (miscellaneous),Astronomy and Astrophysics

Link

http://link.springer.com/content/pdf/10.1007/BF00627766.pdf

Reference8 articles.

1. Engels, R. C. and Junkins, J. L.: 1981,Celest. Mech. 24, 3?21.

2. Hough, M. E.: 1981,Celest. Mech. 25, 111.

3. Jezewski, D. J.: 1983,Celest. Mech. 30, 343?361.

4. Junkins, J. L., Kraige, L. G., Engels, R. C., and Ziems, L.: 1980,Regularized Integration of Gravity Perturbed Trajectories, Virginia Polytechnic Institute and State Univ., Blacksburg Virginia Contract No. N60921-78-C-A214.

5. Mittleman, Don and Jezewski, Don: 1982,Celest. Mech. 28, 401.

Cited by 2 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. DROMO propagator revisited;Celestial Mechanics and Dynamical Astronomy;2015-09-01

2. A special perturbation method in orbital dynamics;Celestial Mechanics and Dynamical Astronomy;2006-12-08

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