<p>We have studied the variations in stability, bifurcation, critical velocity, Lagrange points, and critical periodic orbits in the context of the transition from the Sitnikov four-body system (as analyzed by Soulis et al. (Celest. Mech. Dyn. Astron. 100:251–266, <CitationRef CitationID="CR17">2008</CitationRef>)) to the Sitnikov five-body system. The incorporation of one primary body results in a reduction in critical velocity and an increase in the number of stability intervals. We applied Floquet’s theory to study the stability/instability of the motion of negligible mass. For this, we assume <InlineEquation ID="IEq1"> <EquationSource Format="MATHML"><math> <msub> <mi>z</mi> <mrow> <mi>i</mi> <mi>n</mi> </mrow> </msub> </math></EquationSource> <EquationSource Format="TEX">$z_{in}$</EquationSource> </InlineEquation> as family parameter and vary it in the interval <InlineEquation ID="IEq2"> <EquationSource Format="MATHML"><math> <mo stretchy="false">[</mo> <mn>0</mn> <mo>,</mo> <mn>10</mn> <mo stretchy="false">]</mo> </math></EquationSource> <EquationSource Format="TEX">$[0, 10]$</EquationSource> </InlineEquation>. Upon slightly perturbing the negligible mass from the z-axis, we obtained 13 Lagrange points. We have determined three-dimensional families of periodic orbits which bifurcate from the critical points/bifurcation points. We observed that the bifurcation points lie within the interval <InlineEquation ID="IEq3"> <EquationSource Format="MATHML"><math> <mo stretchy="false">[</mo> <mn>1.0709360</mn> <mo>,</mo> <mn>2.7944120</mn> <mo stretchy="false">]</mo> </math></EquationSource> <EquationSource Format="TEX">$[1.0709360, 2.7944120]$</EquationSource> </InlineEquation>. We have discussed stability/instability of periodic orbits bifurcating from the critical points.</p>

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Stability and bifurcations of symmetrical 3D-periodic orbits in the Sitnikov five-body problem

  • L. P. Pandey,
  • Binay Kumar Sharma,
  • Rahul Tomar

摘要

We have studied the variations in stability, bifurcation, critical velocity, Lagrange points, and critical periodic orbits in the context of the transition from the Sitnikov four-body system (as analyzed by Soulis et al. (Celest. Mech. Dyn. Astron. 100:251–266, 2008)) to the Sitnikov five-body system. The incorporation of one primary body results in a reduction in critical velocity and an increase in the number of stability intervals. We applied Floquet’s theory to study the stability/instability of the motion of negligible mass. For this, we assume z i n $z_{in}$ as family parameter and vary it in the interval [ 0 , 10 ] $[0, 10]$ . Upon slightly perturbing the negligible mass from the z-axis, we obtained 13 Lagrange points. We have determined three-dimensional families of periodic orbits which bifurcate from the critical points/bifurcation points. We observed that the bifurcation points lie within the interval [ 1.0709360 , 2.7944120 ] $[1.0709360, 2.7944120]$ . We have discussed stability/instability of periodic orbits bifurcating from the critical points.