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Research Article Open Access

Lunisolar Invariant Relative Orbits

Walid Ali Rahoma1
  • 1 Department of Astronomy and Space Science, Faculty of Science, Cairo University, 12613, Egypt

Abstract

The present study deal with constructing an analytical model within Hamiltonian formulation to design invariant relative orbits due to the perturbation of J2 and the lunisolar attraction. To fade the secular drift separation over the time between two neighboring orbits, two second order conditions that guarantee that drift are derived and enforced to be equal.

American Journal of Applied Sciences
Volume 10 No. 4, 2013, 307-312

DOI: https://doi.org/10.3844/ajassp.2013.307.312

Submitted On: 7 May 2012 Published On: 2 April 2013

How to Cite: Rahoma, W. A. (2013). Lunisolar Invariant Relative Orbits. American Journal of Applied Sciences, 10(4), 307-312. https://doi.org/10.3844/ajassp.2013.307.312

Open AccessCopyright: © 2013 Walid Ali Rahoma. This is an open access article distributed under the terms of the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original author and source are credited.

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Keywords

  • Formation Flying
  • Invariant Relative Orbits
  • Secular Drift
  • Second Order Conditions
  • Neighboring Orbits
  • Lunisolar Attraction