Lunisolar Invariant Relative Orbits
Walid Ali Rahoma1 Show affiliations
- Department of Astronomy and Space Science, Faculty of Science, Cairo University, 12613, Egypt
American Journal of Applied Sciences, Volume 10, Issue 4, pp. 307–312 · doi.org/10.3844/ajassp.2013.307.312
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.
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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
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