Angela Perdiou

Dr. Angela Perdiou


Research Focus & Metrics

Academic Career Length

22Years (2005-Present)

(Calculated once Scilit publication data is synced: current year − year of first publication + 1)

Representative Publications

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13 June 2008 in Astrophysics and Space Science
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VKV. S. Kalantonis
V. S. Kalantonis
EPE. A. Perdios
E. A. Perdios
APAngela Perdiou
Angela Perdiou

16 June 2012 in Astrophysics and Space Science
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APAngela Perdiou
Angela Perdiou
EPE. A. Perdios
E. A. Perdios
VKV. S. Kalantonis
V. S. Kalantonis

1 October 2005 in Earth, Moon, and Planets
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APAngela Perdiou
Angela Perdiou
VMV.V. Markellos
V.V. Markellos
CDC.N. Douskos
C.N. Douskos

13 June 2008 in Astrophysics and Space Science
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Journal Article
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MMM. P. Markakis
M. P. Markakis
APAngela Perdiou
Angela Perdiou
CDC. N. Douskos
C. N. Douskos

7 June 2021 in Advances in Astronomy
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Elbaz I. AbouelmagdElbaz I. Abouelmagd
Elbaz I. Abouelmagd
VKVassilis Kalantonis
Vassilis Kalantonis
APAngela Perdiou
Angela Perdiou
In this paper, we present a modified version of Hill’s dynamical system that is called the quantized Hill’s three-body problem in the sense that the equations of motion for the classical Hill’s problem are now derived under the effects of quantum corrections. To do so, the position variables and the parameters that correspond to the quantum corrections of the respective quantized three-body problem are scaled appropriately, and then by taking the limit when the parameter of mass ratio tends to zero, we obtain the relevant equations of motion for the spatial quantized Hill’s problem. Furthermore, the Hamiltonian formula and related equations of motion are also derived.

29 November 2016 in The Astrophysical Journal Supplement Series
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JSJagadish Singh
Jagadish Singh
VKVassilis Kalantonis
Vassilis Kalantonis
JGJessica Mrumun Gyegwe
Jessica Mrumun Gyegwe
APAngela Perdiou
Angela Perdiou
We consider a modification of the restricted three-body problem where the primary (more massive body) is a triaxial rigid body and the secondary (less massive body) is an oblate spheroid and study periodic motions around the collinear equilibrium points. The locations of these points are first determined for 10 combinations of the parameters of the problem. In all 10 cases, the collinear equilibrium points are found to be unstable, as in the classical problem, and the Lyapunov periodic orbits around them have been computed accurately by applying known corrector–predictor algorithms. An extensive study on the families of three-dimensional periodic orbits emanating from these points has also been done. To find suitable starting points, for all the computed families, semianalytical solutions have been obtained, for both two- and three-dimensional cases, around the collinear equilibrium points using the Lindstedt–Poincaré method. Finally, the stability of all computed periodic orbits has been studied.