An exact and a new first-order solution for the relative trajectories of a probe ejected from a space station-Reference-Cited by-同舟云学术

An exact and a new first-order solution for the relative trajectories of a probe ejected from a space station

Published:1976-02 Issue:1 Volume:13 Page:75-88
ISSN:0008-8714
Container-title:Celestial Mechanics
language:en
Short-container-title:Celestial Mechanics

Author:

Berreen T. F.,Crisp J. D. C.

Publisher

Springer Science and Business Media LLC

Subject

Space and Planetary Science,Astronomy and Astrophysics,Applied Mathematics,Computational Mathematics,Mathematical Physics,Modelling and Simulation,General Medicine

Link

http://link.springer.com/content/pdf/10.1007/BF01228535.pdf

Reference17 articles.

1. Anthony, M. L. and Sasaki, F. T.: 1965),AIAA J. 3, 1666?1673.

2. Berreen, T. F.: 1973,On the Relative Trajectories of a Probe Ejected from an Orbiting Space Station, Monash University, Ph.D. Thesis, Ch. 3.

3. Crisp, J. D. C.: 1962,Astronautica Acta VIII, 1?27.

4. De Vries, J. P.: 1963,AIAA J. 1, 2626?2629.

5. Eades, J. B., Jr.: 1972,Relative Motion of Orbiting Satellites, Analytical Mechanics Associates Inc. Maryland, Report 72-27.

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